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 DALA2025121209101Longeron · crackedCRACK IN WTB FAIRING LONGERON P/N 53-1111-501 AT LBL 40.0. CRACK SPREAD BETWEEN TWO NUT PLATES ON OUTBOARD SIDE OF LONGERON FORWARD OF FRAME AT FS 973. CRACK MEASURES 6 1/8" LONG BY 1/2 " WIDE. AD RELATED REF WORK CARD 5352-01038-01A. COMPLIED WITH WORK CARD 5SDR SWAA2025121242831Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 1192; 4' LEFT OF TOP. CRACK LENGTH, L=4' W=2.5'. THE TAIL CONE WAS REMOVED AND REPLACED WITH A NESDR SWAA2025121242832Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. BS 1193.5; 24.5' RIGHT OF TOP. CRACK LENGTH, L=3' W=1.5'. THE TAIL CONE WAS REMOVED AND REPLACED WITH A NEW SDR SWAA2025121246031Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 1192; 4 INCHES LT OF TOP. CRACK LENGTH, L=4' W=2.5'. TAIL CONE R & R WITH A NEW ONE.SDR SWAA2025121246032Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID, BS 1193.5; 24.5' RT OF TOP. CRACK LENGTH, L=3' W=1.5'. TAIL CONE R & R WITH A NEW ONE.SDR SWAA2025121242833Tail Cone · delaminatedTHE FORWARD TAIL CONE FAIRING IS DELAMINATED, BS 1190 21 INCHES RIGHT OF TOP. CRACK LENGTH: L=2.3' W=2.2'. LOCATED & DRILLED INITIAL TAIL CONE SCREW HOLES WITH EXCEPTION OF HOLES AROUND ELEVATOR PUSH ROD CUT OUTS IAW MM 51-40-02 & SIP. TAIL CONE WAS R & R SDR SWAA2025122942478Former · crackedWING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGERS 19 & 20R. REMOVED AND REPLACED FAIRING FORMER ON WING BODY BS 500D BETWEEN S19 AND S20R IAW SRM 51-40-02; 51-40-05 AND DWG 116A3010 REV A.SDR CALA2025120511807Bracket · crackedONE BRACKET CRACKED AT THE LOWER LEFT WING OT BODY FAIRING STRUCTURE AT BS 1040, LOCATED AT THE FWD END OF THE BEAM. REMOVED AND REPLACED THE BRACKET ON LT WTB FAIRING STRUCTURE AT BS 1040 IAW SRM 51-40-02-0G. & DWG 149N7553.SDR VNAA202512020009Frame · corrodedWING TO FUSELAGE FAIRING FRAME IS CORRODED AT STGR 27.SDR SWAA2025120442290Boot · crackedNOSE RADOME BOOT CRACKED. REPLACED NOSE RADOME BOOT IAW AMM 53-52-00.SDR SWAA2025120441560Tail Cone · delaminatedTAIL CONE RT SIDE HAS SKIN DELAMINATION JUST FORWARD AND BELOW THE TAIL CONE ACCESS DOOR NEAR BS 1190. COMPLIED WITH 25-153-03292 (COMPONENT - REPAIR - FUSELAGE SECTION 48 DISBONDING COMMON TO TAIL CONE.SDR SWIA2025120175727Skin · chafedLEFT APRON SKIN CHAFED WHERE IT MEETS THE WING. REMOVED DAMAGE ON LT APRON SKIN WHERE IT MEETS THE WING. CUT AWAY DAMAGED PORTION OF LT APRON SKIN PANEL. FABRICATED REPLACEMENT AND WET INSTALLED. APPLIED CIC AND PRIMER. PER REO 601R-53-41-115 REV -A, COMPLETESDR SWAA2026011341328Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BS 500I, S19R BELLY FAIRING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 116A3110, SHEET 8, REV -, AND DWG 149A7101, SHEET 11, REV -.SDR JR2R20251201487Cone · brokenAFT WING-TO-BODY FAIRING, CONE ASSEMBLY IS BROKEN IN TWO PLACES. REPAIRED.SDR VNAA20260511022Strap · corrodedFS 629 WING-TO-FUSELAGE FAIRING SUPPORT STRAP IS CORRODED ON THE LOWER SIDE. INSTALLED NEW WING-TO-FUSELAGE FAIRING SUPPORT STRAP (P/N SH670-39054-3) AT FS 629 IAW CRJ-700 SRM 51-23-00-001-001-A01 AND CRJ-700 SRM 51-25-16-001-001-A01.SDR SWAA2026011347401Access Panel · crackedCRACK WING TO BODY FAIRING ACCESS PANEL 194BR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-10, REPAIR 10.SDR SWAA2026010840487Access Panel · crackedCRACK WING TO BODY FAIRING ACCESS PANEL 194BR AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 194BR IAW SRM 51-70-05-2R-10 REPAIR 10.SDR DALA2025121609150Tail Cone · missingON WALK AROUND FOUND APU TAILCONE MISSING. PERFORMED SPLICE REPAIR ON WIRE 3348-7875 FROM 18LV IN THE FORWARD TAILCONE AREA. ALSO ROUTED HARNESS & SECURED GROUNDS, IAW ESPM 2347890-53-02-0201. REMOVED TAILCONE IAW AMM 53-58-11. REMOVED APU IAW AMM 49-11-11. SDR REXA2026052700737Hinge · corrodedCORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR WAS EVALUATED OUT OFF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND HINGES AND FITTINGS WERE REPSDR REXA2026052700736Hinge · corrodedCORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR WAS EVALUATED OUT OFF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND HINGES AND FITTINGS WERE REPSDR REXA2026052700735Hinge · corrodedCORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR CORROSION ON HINGES (2EA) AND HINGE FITTINGS (2EA) AT ACCESS FAIRING PANEL 196DR WAS EVALUATED OUT OFF LIMITS PER SRM 51-10-06-001-001-A01 AND HINGES AND FITTINGS WERE REPLACED PSDR QMLA2025112420116Tail Cone · crackedCRACKS DISCOVERED IN TAIL CONE STATION 6616 DURING 1600 HOUR INSPECTION. AMC EO 32-5302-EO-2290 PREVIOUSLY COMPLIED WITH.SDR SWIA2026031875536Skin · chafedTHE APRON SKIN UNDER THE LT STUB FAIRING IS CHAFED. REPAIRED THE APRON SKIN UNDER THE LT STUB FAIRING BY CUTTING OUT THE DAMAGED PORTION AND REPLACING WITH NEW SKIN PANEL IAW REO 601R-53-41-115, REV -A.SDR SWAA2025122941132Former · wornRIGHT LOWER FAIRING FORMER AT BS 663 - 673, RBL 20, WL 142 WORN ON LOWER SIDE OF FORMER. REMOVED AND REPLACED THE RT LOWER FAIRING FORMER IAW SRM 51-40-02-0G0, AND DWG 149A7216, REV A.SDR SWAA2025122941131Former · wornLEFT LOWER FAIRING FORMER, BS 663 - 673, LBL 20, WL 142 WORN ON LOWER SIDE. REMOVED AND REPLACED THE LT LOWER FAIRING FORMER IAW SRM 51-40-02, DWG 149A7216, REV:A.SDR SWAA2025121638625Access Panel · delaminatedDELAMINATED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL ON THE BODY FAIRING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR CALA2025112411428Support Rib · crackedFOUND CRACK LT WING TO BODY FAIRING SUPPORT RIB INBD OF FRONT SPAR FIXED L/E FAIRING BS 500. REMOVED DAMAGE PART AND INSTALLED NEW LT WING TO BODY FAIRING SUPPORT RIB INBD OF FRONT SPAR FIXED L/E FAIRING BS 500 IAW SRM 51-40-02-0G-0, DWG 116A3110 AND 116A30SDR IXXA03142026CC01Frame · corrodedRH AFT WING TO BODY FAIRING ATTACH FRAME AT STA 1220 IS CORRODED.SDR DALA2025122609411Seal · detachedFLIGHT ATTENDANT AND PASSENGERS REPORT A LOUD NOISE IN CENTER CABIN. SEEMS LOUDEST NEAR LEFT O.W. EXIT.FOUND SEAL ON WING TO BODY FAIRING PANEL 193EB DETERIORATED. APPLIED ER/A 603214-14TR REV B. C/W SECTION I: TIME LIMITED REPAIR AND APPLIED SPEED TAPE. ASSOCSDR DALA2025112008498Radome · damagedSHIP 3237 DISC: BIRD STRIKE ON LOWER NOSE CONE ON CA SIDE. ABOUT 7500' ON CLIMB OUT FROM DENVER. NO ADVERSE CONDITIONS EXPERIENCED. C/A: INSPECTED A/C PER A320 AMM 05-51-14-200-803. DAMAGE NOTED ON RADOME. NO FURTHER DAMAGE ON A/C (WIP 184199) R&R RADOME PER ASDR IXXA04082026CC01Angle · corrodedRH AFT LOWER WING TO BODY FAIRING FRAME STA 1050 IS CORRODED.SDR IXXA20262026002Support Bracket · corrodedLEFT LOWER WING - BODY FAIRING SUPPORT BRACKET STA 958 IS CORRODED.SDR VNAA202601180012Strap · crackedCORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESSPANEL 193AB. SUPPORT STRUCTURE STRAP FAIRING ACCESS PANEL 193AL AND 193AR WERE REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01SDR VNAA202601180010Bracket · corrodedCORROSION ON INTERNAL ANGLES OF REFUEL/DEFUEL CONTROL PANEL SUPPORT STRUCTURE. CORROSION ON INTERNAL ANGLE P/N: CC670-39182-8 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101- 001-A01 AND ANGLE 1EA (BRSDR SWAA2025122235374Access 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. SSDR SWAA2025122234830Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 192HR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 192HR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025122234831Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 192AR BODY FAIRING AT FUSELAGE EXTERIOR . REPAIRED ACCESS PANEL 192AR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025122234826Access Panel · elongatedELONGATED HOLE ACCESS PANEL 192AL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 192AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-9 REPAIR 9.SDR SWAA2025122234469Access Panel · crackedCRACKED ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10.SDR SWAA2025120334104Support · crackedRIGHT WING TO BODY FORMER SUPPORT CRACKED JUST INBD OF FIXED L/E BS 500D, S19R, ACCESS PANEL 191FR. REMOVED AND REPLACED THE WING TO BODY FORMER SUPPORT IAW SRM 51-40-02, AND DWG: 116A3010 REV -.SDR AALA202512039318Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK BRACKET ANGLE AT BELLY FAIRING AT LEVEL OF BS 1035 RIGHT HAND SIDE AT LOWER FUSELAGE. REPLACED BRACKET ASSEMBLY. PER B777 AMM 28-11-00-300-802 STEP F(8), B777-200 SRM 51-40-02-0G AND DRAWING 112W4301 (SHEET 17) REV A.SDR JGVR20251111002Tail Cone · corrodedREPAIRED CORRODED AREA LOWER TAILCONE SKINS AT THE AIRCRAFT DATA PLATE BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ENGINEERING REPAIR ORDER.SDR CALA2025111311176Radome · damagedLARGE BANG CLIMBING TRU 8000 NO ABNORMALITIES CREW REPORTS A LOUD BANG AT 8,000 FT WITH NO OTHER ABNORMAL ISSUES. CREW ALSO REPORTS NO OVERWEIGHT OR HARD LANDING. UPON ARRIVAL BACK TO IAD, DISCOVERED A LARGE BIRDSTRIKE ON THE UPPER LT SIDE OF NOSE RADOME AREA.SDR DALA2025111108223Radome · delaminatedDURING BIRDSTRIKE INSPECTION FOUD DELAMINATION & BUBBLE ON THE INSIDE OF RADOME NOSE. REMOVED NOSE RADOME IAW AMM 53-15. INSTALLED RADOME IAW AMM 53-15-11. OK FOR SVC. (LP: 7726841)SDR DALA2025111008208Access Panel · erodedEROSION ACCESS PANEL 191DB AT LOWER FUSELAGE. COMPLIED WITH ER/A 629770-14. (1296589).SDR SWAA2025120333428Panel · delaminatedPANEL 194CR HAS DELAMINAION ON OUTER SURFACE. PANEL 194CR WITH DELAMINATION ON OUTER SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-60-70-2R-1.SDR SWAA2025120333427Panel · delaminatedPANEL 194CL HAS DELAMINAION ON OUTER SURFACE. REPAIRED IAW AMM 51-21-99-300-802.SDR CALA2025110510916Fairing · damagedHUMMING NOISE COMING FROM ENG 2 SIDE EXIT ROW AT CRUISE. ENG AND PRESS INDICATIONS NORMAL, OK TO PLACE ON CARRY PER MT -53-004 ACCOMPLISHED INTERIM REPAIR AND APPLIED SPEED TAPE TO WING TO BODY PANEL RIGHT SIDE 192DT.SDR SWAA2025112831420Access Panel · delaminatedDELAMINATED ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-2 REPAIR 2.SDR VNAA20251204007Support · corrodedAFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STRINGER 22R AND 21R. FT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40 BTW STRINGER 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-04
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