JASC 5350
Service difficulty reports · 6,115
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 R61A2026092600272Strap · corrodedDURING HEAVY CHECK MAINTENANCE FOUND AFT WTF FAIRING ATTACHMENT STRAP BETWEEN FR 73- 75, STR 23L - 29L CORRODED. WTBF FAIRING ATTACHMENT STRAP WAS REMOVED AND REPLACED IAW SRM 51-43-04 AND 51-41-02.SDR R61A2026092600271Support · corrodedDURING HEAVY CHECK MAINTENANCE FOUND WTB FAIRING RIB LT & RT SUPPORT CORRODED AT CFII FR54. THE WTB FAIRING RIB SUPPORT WAS REPLACED IAW SRM 51-41-02, AND 51-42-02.SDR R61A2026092600262Strap · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND CORRODED FWD WTB FAIRING TO FUSELAGE STRAP FOUND ON CFII AT FR 27-28, STR 24R-28L. THE FWD WTB FAIRING TO FUSELAGE STRAP WAS REPLACED IAW SRM 51-42-02, SRM 51-43-04 AND SRM 51-41-02.SDR SWAA2026090169727Panel · delaminatedPANEL 193CL LEADING EDGE HAS AREA OF EROSION AND DELAMINATION. R & R PANEL 193CL PER AMM 53-51-21.SDR DALA2026082604830Radome · damagedBIRD STRIKE ON LANDING ROLL NO ABNORMAL ENGINE INDICATIONS OR ODOR. C/W BIRD STRIKE INSPECTION, REMAINS REMOVED IAW AMM 05-51-14, FOUND PERFORATION DAMAGE TO RADOME APPLIED REPAIR IAW AMM 53-15-11. ACFT OK FOR SERVICE. (LP: 9318514, AIRCRAFT WAS GROUNDED)SDR SWAA2026092192325Rub Strip · gougedGOUGED RUB STRIP ON THE BODY FAIRING LOWER ANGLE, BS 540 + 10 INCHES AND RBL 41. REPAIRED THE RUB STRIP IAW SRM 57-10-13-2R-3.SDR CALA2026082118781Support Frame · crackedCRACKED LT WING-TO-BODY FAIRING SUPPORT FRAME CRACKED. R & R SUPPORT FRAME AT LT WING TO BODY FAIRING PANEL NR 191AL IAW SRM 51-40-02-0G-0, AND DWG 116A3010, SHEET 21.SDR CALA2026082018754Support Frame · crackedCRACKED RT WING-TO-BODY FAIRING SUPPORT FRAME, AT ACCESS PANEL 191BL. R & R THE SUPPORT FRAME AT RT WING TO BODY FAIRING ACCESS PANEL 191AR IAW SRM 51-40-02-0G-0, & DRAWING 116A3010 SHEET 21.SDR SWAA2026092873584Panel · debondedPANEL 192BR OUTER SKIN IS DISBONDED NEAR THE FWD EDGE. THE PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR IPXA2026090413630Radome · erodedRADOME HAS EROSION ON CAPTAIN€™S SIDE. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 100 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. INSTALL RADOME BOOT I.A.W. UPS EO-35385-JIC001 REV. 4. I.A.W AMM 53-12-01-SDR IPXA2026092805342Rib · crackedFAIRING 475AL, FWD I/B RIB CRACK. REMOVED AND REPLACED NEW RIB ON FAIRING 475AL, FWD I/B IAW SRM 51-40-21.SDR JR2R20260815234Attach Angle · corrodedWING TO BODY LANDING AT FR 52 IS CORRODED OUT OF LIMITS. REPLACED.SDR VNAA202608200002Tail Cone · dentedDENT IN TAILCONE WAS REPAIRED IAW REO 690-53-84-062 REV -.SDR SWAA2026091070928Panel · debondedDISBOND ON OUTER SURFACE OF PANEL 193AR 04 - REPAIRED PER SRM 51-70-05-2R-1-A00732, REPAIR 1. REPAIR OF DAMAGE TO ONE SKIN OF A HONEYCOMB PANEL, AIRFRAME PERMANENT.SDR N6WA2026081202Support Angle · corrodedCORROSION ON FWD FUSE FAIRING SUPPORT TEE ATTACHMENT AT BS 629 - 661 NEEDS EVALUATED. REMOVED AND REPLACED FWD FUSELAGE FAIRING SUPPORT TEE ATTACHMENT AT BS 629 - 661 IAW SRM 51-42-06.SDR U2RA202609070005Frame · crackedR/H WING TO BODY FAIRING (STA 880 ) STRUCTURE CRACK ON FRAME ASSY AT BSTA 800, RBL 125,WL 180 PERMANENT REPAIR PER B747 SRM 53-00-71 REPAIR A. WITHOUT DEVIATIONS FAA FORM 8100-9 ISSUEDSDR IPXA2026092127542Support · crackedLEFT FR 47 HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE "P" IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).SDR IPXA2026092127516Support · crackedLEFT FR47 HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE "D" IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).SDR IPXA2026092127471Support · crackedLEFT FR 47, HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE B IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).SDR IPXA2026083102323Support Bracket · brokenFOUND LEFT TAIL CONE SUPPORT BRACKET BROKEN BS 2460, LBL 36. REMOVED THE DAMAGED SUPPORT BRACKET IAW SRM 51-40-02-0G, REV 49. INSTALLED A FABRICATED BRACKET IAW SRM 51-40-02-0G, REV 49, & DWG 148U2460, SH31, REV-.SDR IPXA2026082402323Support Bracket · brokenFOUND LT TAIL CONE SUPPORT BRACKET BROKEN BS 2460, LBL 36.SDR DALA2026081004612Support · wornAFTER EVALUATING THE BARE METAL ON THE AFT FAIRING SUPPORT LOCATED AT FR61 BETWEEN RBL 10 TO LBL 10 FOUND CORROSION. NO DAMAGE IS ALLOWED IAW ASRP BD500-A-J53-82-08-00AAA-661A-A, FIG 2. REPLACED THE FAIRING SUPPORT IAW PL C01731500 REV-E AND ASRP BD500-A-J51SDR IPXA2026080842558Fairing · debondedDEBONDED SKIN, RT AFT WING TO BODY FAIRING EXTERNAL, PANEL 198CR. IAW SRM 52-40-02-2R-4, REF SRM 51-70-17-0G-0, & SRM 51-70-14-0G-0, REV 95. REMOVED DEBONDED MATERIAL & CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 200F FOR 220 MINUTES WITH MINIMUM VASDR YENA2026080700661Seal · damagedFLT 1707, FLL-LAS. ABNORMAL VIBRATION AND LOUD HUMMING SOUND CONCENTRATED IN MID CABIN AROUND ROW 11- BOTH SIDES OF THE AIRCRAFT REPORTED B Y FA AND DH PILOTS IN CABIN - SUBTLE VIBRATION ROW 10-18; ACCOMPLISHED VIBRATION INSP TSM 05-50-00-810-801 AND IDENTIFIESDR DALA2026081204639Fairing · dentedRIGHT AFT WTB PANEL 194GR HAS A DENT. REPAIRED RT AFT WING TO BODY FAIRING 194 GR IAW SRM 53-60- 70-2R, REPAIR 1. (1738855) AIRCRAFT WAS GROUNDEDSDR REXA2026091101812Access Panel · corrodedCORROSION ON NUTS STRIP OF BODY FAIRING ACCESS PANEL 194AB. 08/02/2026 STRIP OF BODY FAIRING ACCESS PANEL 194AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01.SDR DALA2026073004413Support Angle · corrodedCORROSION ON WTB SUPPORT ANGLE FROM FR-30+12 TO FR-34+15, BETWEEN STR- 36L AND STR- 30L. REMOVED AND REPLACED WTB SUPPORT ANGLE FROM FR- 30+12" TO FR-34+ 15" BETWEEN STR-36L AND STR-30L PER A220 ASRP BD500-A-J51-42-06- 00AAA-078A-A STEP 6 AND A220 ASRP BD500-ASDR HNAA2026081900737Angle · crackedLWR FUSE BODY FAIRING 192EL, WING STUB LT FWD RETAING ANGLE L SHAPE CRACKED. REPAIRED IAW SRM 57-20-01SDR IPXA2026081872380Skin · corrodedAFTER CLEANING, FOUND CORROSION ON APU TAIL CONE SKIN PANEL AT STA.1963.8 VERIFIED STEP 13 NO REPEAT INSPECTION. REPAIR DOUBLERS FROM MATERIAL REF SRM 53-80-01-01 DETAIL II, B757 SRM 51-70-10-2R-0 PARA, 8.A.SDR JR2R20260725787Landing · bentFORWARD LANDING FOR PANEL 351GL IS BENT. REPAIRED PER ETD.SDR IPXA2026090432341Skin Panel · damagedAFT SIDE OF FRAME STA 1963 AND LOWER METAL HONEYCOMB SKIN PANEL LEVELING COMPOUND AROUND DRAIN HOLES SEPERATED FROM CORRODED STRUCTURE. RL038 INSTALLED SKIN AT PANEL AT STA 1963 IAW SRM 51-40-02-OG-0SDR IPXA2026090431507Doubler · corrodedTAIL CONE STA 1992 FRAME FWD AND AFT SIDES HAVE AREAS OF CORROSION AND AREAS OF PROTECTIVE FINISH BLISTERING UP AND PEELING OFF CIRCUMFERENTIALLY AROUND FRAME. RL033 INSTALLED FRAME (RING) AT TAIL CONE STA 1992 IAW SRM 51-40-02-0G-0.SDR CALA2026072417968Panel · missingLEFT WING TO BODY FAIRING PANEL 191DT FOUND MISSING UPON LANDING. REMOVED REMAINING PANEL AND INSTALLED NEW PANEL IAW MM 53-35-11.SDR MASA20260807205Retainer · corrodedDURING HEAVY CHECK INSPECTIONS FOR CFIII FR74 LBL 15 - RBL 15 FOUND CORROSION ON AFT WTB RETAINER STRAP HAS BEEN REMOVED BY BLENDING OUT IAW SRM 51-10-03 FOUND WITHIN LIMITS IAW SRM 53-04-02 AD 02 REV 45 MAY 28 21 GVI ON REWORKED AREA WITH MAGNIFIENT 10X NO FASDR JR2R20260721771Fairing · corrodedW/B PANEL 195HL BLISTER FLAP DOOR HAS CORROSION SPOTS. REPAIRED PER ETD.SDR R61A2026072000195Radome · damagedDROP IN - DAMAGE TO NOSE AT RADOME. REPLACED FR 1 AND GUTTER SRM 51-40-08 AND COMPLIED WITH ETD2026-170-012441 AND ETD2026-170-012474 FOR PERMANENT REPAIR OF NOSE DAMAGE ON RH SIDE AT RADOMESDR IPXA2026081624489Channel · crackedRIGHT HORIZONTAL STAB LOWER SLIDING FAIRING LEADING EDGE GUIDE CHANNEL LOWER AND MIDDLE SECTIONS ATTACHED TO FUSELAGE WORN THIN AND CRACKED. INSTALLED NEW TRACK RH HORZ STAB SLIDING FAIRING IAW SRM 51-40-02-0G-0 PAR. 4 AND 7 REV 125 20.SDR IPXA2026081530937Support Bracket · crackedRIGHT AFT WTB LOWER PANEL LANDING SUPPORT BRACKET HAS EVIDENCE OF CRACK AT RADIUS. INSTALED NEW WTB LOWER PANEL LANDING SUPPORT BRACKET IAW SRM 51-40-02-0G-0.SDR IPXA2026081130876Support Bracket · crackedLEFT AFT WTB PANEL LANDING SUPPORT BRACKET HAS EVIDENCE OF CRACK AT THE RADIUS. INSTALLED NEW SUPPORT BRACKET ON LH AFT WTB PANEL STRUCTURE IAW SRM 51-40-02-OG-O.SDR IPXA2026081130875Support Bracket · crackedRIGHT AFT WTB UPPER PANEL LANDING SUPPORT BRACKET HAS EVIDENCE OF CRACK AT RADIUS. INSTALLED NEW SUPPORT BRACKET AT AFT UPPER WTB RAIRING FRAME STRUCTURE IAW B757-200 SRM 51-40-02-OG-0SDR IPXA2026091101707Skin · corrodedAPU COMPARTMENT TAILCONE LOWER BILGE ALUMINUM HONEYCOMB SKIN PANELS BETWEEN BS 1963 AND 1992 HAS AREAS OF CORROSION TO INCLUDE ATTACHMENT TO FRAMES WITH AREAS OF MISSING FINISH. RL051 RE-INSTALLED LWR BILGE ALUM HONEYCOMB SKIN PNL BTWN STA 1963 & 1992 AT APU CSDR HNAA2026082400776Support · crackedRIGHT CTR FUSE 3, AT FR 42, WING TO FUSELAGE FAIRING SUPPORT CRACKED. REPAIRED IAW SRM 53-23-12SDR DALA2026071304128Tail Cone · damagedTAIL CONE HAS MULTIPLE LIGHTNING STRIKES BEYOND ALLOWABLE LIMITS. REPLACED TAIL CONE IAW AMDS W/C 5352-4013. (9204003) (AIRCRAFT GROUNDED)SDR SWAA2026081266013Access Panel · delaminatedDELAMINATED ACCESS PANEL 194FL, LOWER BELLY FAIRING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-2, REPAIR 2.SDR YENA2026071500577Tail Cone · crackedDURING HEAVY MAINTENANCE, FUSELAGE TAIL CONE, FR 81-84 & STR 15 CORRODED & CRACKED. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR DALA2026071004045Fairing · missingRIGHT WING .5 ROOT FILLET FAIRING MISSING. DEFERRED RT ROOT FILLET FAIRING PER A320 CDL 53-00-03. M PROCEDURE C/W. PLACARD INSTALLED. (LP: 8820352, AIRCRAFT WAS GROUNDED)SDR VNAA202609010018Hinge Fitting · corrodedCORROSION ON HINGE FITTINGS (2 EAS) OF ACCESS DOOR AT FAIRING 196DR. HINGE FITTINGS (2 EAS) OF ACCESS DOOR AT FAIRING 196DR WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801-A01SDR DALA2026070603939Support Bracket · wornWORN SPRING SUPPORT BRACKET & PULLEY BRACKET OF RELEASE MECHANISM AT TAIL CONE. SPRING SUPPORT BRACKET, SPRING RELEASE MECHANISM & PULLEY BRACKET OF RELEASE MECHANISM AT TAIL CONE WERE REPLACED IAW AMM 20-50-01 AND SRM 51-41-01-0G. (1682506)(AIRCRAFT GROUNDED)SDR DALA2026070403904Radome · damagedATB DUE TO BIRD STRIKE. FOUND RADOME DAMAGED. REPLACED RADOME PER AMM 53-15-11. OPS TEST OF WEATHER RADAR OK. (LP 8527430, 8527431 - AIRCRAFT WAS GROUNDED)SDR DALA2026082504828Longeron · corrodedER/A 635349-14; A220-100 / FWD & CNTR WING TO BODY FAIRING / MULTIPLE LONGERON / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 635349-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 12,873 TOTAL AIRCRAFT FLIGHT HOURS
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