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 AALA202508256622Fairing · looseAIRCRAFT WAS GROUNDED: OVERWEIGHT LANDING. EMERGENCY DECLARED. LANDING WEIGHT 140,100. PASSENGERS AND FA REPORTED LOUD BANGING NOISE ON RIGHT SIDE OF AIRCRAFT, NEAR THE FLOOR, COMING FROM THE OUTSIDE. MOC REQUESTED RETURN TO DFW. FOUND SPEED TAPE ON RH WING FAAug 24, 2025 · N4005X · Airbus A319115SDR SWAA2025100607409Access Panel · crackedCRACK ON HOLES ACCESS PANEL 193AR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCES PANEL 193AR IAW SRM 51-70-05-2R-10 REPAIR 10 .Aug 22, 2025 · N901WN · Boeing 7377H4SDR SWAA2025100607408Access Panel · crackedCRACK ON HOLES 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.Aug 22, 2025 · N901WN · Boeing 7377H4SDR HNAA2025090800588Skin · crackedREAR FUSELAGE 1 LH UPPER SKIN RIVET AT FR76, STRG 6L IS POSSIBLE CRACKED. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 1LH UPPER SKIN AT FR 76 STRG 6L IAW ETD2025-145-926199 / EO1-53-25-0283.Aug 21, 2025 · N646AE · Emb EMB145LRSDR IPXA2025091564404Tail Cone · damagedMAJOR REPAIR, DAMAGE ON TOP OF TAILCONE AREA BELOW RUDDER ALL STEPS OF EO-94785-REQ2 COMPLETED. THIS DEFERRAL IS NOW CLOSED.Aug 20, 2025 · N406UP · Boeing 75724APFSDR IPXA2025090530455Radome · dentedLEFT FWD SIDE OF FUSELAGE HAS A DENT AFT OF RAYDOME AT APPROX FS 205 L24L . 49-001 ATA 53-00. INSTALLED 1EA (-1) REPAIR DOUBLER AND 1EA (-2) FILLER ON L/H FWD SIDE OF FUSELAGE AFT OF RAYDOME AT APPROX FS L24L IAW E.A.#:757-5310-01-B0557 REV:P1, STEP 22 AND 2Aug 18, 2025 · N436UP · Boeing 75724APFSDR DALA2025081906216Support · gougedTHREE GOUGES ON WTBF SUPPORT STRUCTURE AT FR38, BETWEEN RBL25 AND RBL30. REMOVED AND REPLACED WING TO BODY SUPPORT P/N: C02381124-002, PO :1049347 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A. AT FR 38 RH SIDE BETWEEN RBL 25 AND RBL 30. (LP# 1145374)Aug 15, 2025 · N126DU · Airbus BD5001A10SDR IPXA2025090270230Tee Fitting · corrodedLEFT AFT BODY FAIRING BS 1220, LBL 65, TEE FITTING HAD CORROSION. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02-0G.Aug 14, 2025 · N466UP · Boeing 75724APFSDR SWAA2025091503714Support · crackedLH WING TO BODY FAIRING SUPPORT HAS CRACKED AROUND THE FASTENER. REMOVED AND REPLACED LT WING TO BODY FAIRING SUPPORT IAW SRM 51-40-02 AND DWG 116A3010 ID: 0039 REV -.Aug 12, 2025 · N904WN · Boeing 7377H4SDR SWAA2025090803538Access Panel · delaminatedDELAMINATED ACCESS PANEL 191FL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 191FL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-6 REPAIR 6 AND SRM 51-70-04-2R-0 REPAIR GENERAL.Aug 12, 2025 · N447WN · Boeing 7377H4SDR SWAA2025091200092Panel · debondedPANEL 193CL HAS LARGE DISBONDS ON BOTH SKINS. DUE TO THE EXTENT OF DAMAGE; REPLACED PANEL 193CL WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-14-00-03A ITEM 290.;Aug 10, 2025 · N224WN · Boeing 7377H4SDR SWAA2025091200093Panel · debondedPANEL 193CR INNER SKIN IS DISBONDED. REPAIRED IAW SRM 51-70-05-2R-2-A00733, REPAIR 2. REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE.Aug 10, 2025 · N224WN · Boeing 7377H4SDR SWIA2025080675195Skin · gougedEXTERNAL LOWER SKIN GOUGED FROM WING-TO-BODY FAIRING AT STRG27, BS 977 - BS 985. BLENDED OUT DAMAGE ON EXTERNAL LOWER SKIN AT STGR27, BS 977 - 985 IAW SRM 51-12-00-001-001-A01 AND COMPLIED WITH NOTES A., B., AND C. OF GREO 670-53-00-290, REV F. LEAK CHECKED GAug 6, 2025 · N685SK · Cndair CL6002C10SDR SWAA2025090999119Panel · delaminatedPANEL 193B HAS DELAMINATION ON OUTER SURFACE. PANEL 193B REPAIRED IAW SRM 51-70-05-2R-2.Aug 6, 2025 · N906WN · Boeing 7377H4SDR UIEA2025072100984Fairing · crackedLONGERON BOX FAIRING FOUND CRACK.(<P>PERFORMED REPAIR AT CRACKED AREA AS PER RI-53-40-17743 REV.A. NO FURTHER DEFECTS NOTED.</P>)Aug 1, 2025 · N856GT · Boeing 74787UFSDR DALA2025080105780Tail Cone · damagedTAILCONE LT FUSELAGE SKIN AT STA1783 UNDER SEAL PANEL 313CLX FOUND ABRASION. DAMAGED AREA REPAIRED PER SRM 53-80-70.Jul 29, 2025 · N834MH · Boeing 767432ERSDR CALA2025073107137Support Angle · crackedLEFT FWD FRONT SPAR WING TO BODY FAIRING AT FIXED L/E I/B SUPPORT ANGLE CRACKED. R & R SUPPORT ANGLE AT LT WING FRONT SPAR WING TO BODY FAIRING AT FIXED L/E I/B SIDE IAW SRM 51-40-02-0G-0.Jul 29, 2025 · N73283 · Boeing 737824SDR R61A2025082000357Strap · corrodedLOWER WING TO FUSE FAIRING STRAP FOUND CORRODED. MX REPLACED STRAP IAW SRM 51-43-04.Jul 28, 2025 · N731YX · Emb ERJ170200LRSDR JJBA20250730109Angle · crackedRH WING TO BODY FAIRING, ANGLE #3 FOUND CRACKED. RH WING TO BODY FAIRING, ANGLE #3 REPLACED.Jul 28, 2025 · N16147 · Emb EMB145XRSDR DALA2025080205798Pin · cockedTAIL CONE RELEASE CAM PIN CLOCKED INCORRECTLY. ADDED WASHERS AND SHIMS WHICH WAS MISSING FROM THE TAIL CONE RELEASE CAM PIN TO CORRECT EXCESSIVE FORWARD AND AFT PLAY IN TAIL MECHANISM RELEASE CAM ASSEMBLY REF B717 AMM 53-52-03.Jul 27, 2025 · N957AT · Boeing 717200SDR DALA2025072805618Tail Cone · ground damageAIRCRAFT 3060, WHILE BEING TOWED TO THE GATE IN PNS, THE SUBJECT A321 TAIL CONE (P/N D0007000510000) WAS DAMAGED WHEN THE LH ELEVATOR ON AIRCRAFT 3060 CONTACTED AN ADJACENT BUILDING. THE TAIL CONE SKIN WAS DENTED, DAMAGING THE UNDERLYING STRUCTURE IN THE AREA Jul 27, 2025 · N360DN · Airbus A321213SDR DALA2025072405556Radome · damagedSHIP 3119 DAMAGE TO NOSE RADOME RIGHT SIDE. CORRECTIVE ACTION: R/R RADOME PER A320 AMM 53-15-11. (1102409)Jul 24, 2025 · N319NB · Airbus A319114SDR CALA2025072406867Radome · crackedPOSSIBLE LIGHTNING STRIKE AND CRACK ON NOSE RADOME. NOSE RADOME REMOVAL REF AMM 53-52-00-000-802 UP TO AND INCLUDING STEP 2A. INSTALLED NOSE RADOME IAW AMM 53-52-00-000-802 OPS CHECK GOOD.Jul 23, 2025 · N27269 · Boeing 7378SDR DALA2025072105477Fairing · puncturedBELLY PANEL 191AB PUNCTURED ALONG FWD EDGE INLINE WITH DRAINMAST. COMPLIED WITH ER/A 628017-14.Jul 21, 2025 · N811NW · Airbus A330323SDR JJBA20250721079Angle · crackedCRACK ON LH WING TO BODY FAIRING LOWER ANGLE #2 AT FR 47. LOWER ANGLE #2 AT LH WING TO BODY FAIRING, FR 47 REMOVED. ANCHOR NUTS ON ANGLE REMOVED. HOLES TRANSFERRED ON NEW ANGLE. ANCHOR NUTS REINSTALLED. NEW ANGLE INSTALLED AND SEALED. SURFACE REPROTECTED.Jul 21, 2025 · N11199 · Emb EMB145XRSDR DALA2025071805435Radome · damagedSHIP 3327 RADOME NEED TO BE REPLACED DUE TO HAIL DAMAGE. REMOVED AND REPLACED RADOME AS PER A330 AMM 53-15-11-400-801-A. (7050215).Jul 16, 2025 · N827NW · Airbus A330302SDR SWAA2025081491393Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 193B, BODY FAIRING AT LOWER FUSELAGE. REPAIRED THE ACCESS PANEL 193B, BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-04-2R-9 REPAIR 9.Jul 14, 2025 · N7826B · Boeing 73779PSDR SWAA2025082290419Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 192HR BODY FAIRING AT FUSELAGE EXTERIOR 2025-447888<[01] EQUIPMENT P/N EPOCH 650; S/N 190776902; DUE DATE 15-OCT-25 WAS USED ON STEP 10;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH8P3/R250; S/N: 16240122 ; DUE DATJul 11, 2025 · N7843A · Boeing 737752SDR DXTA2025071404189Panel · looseINFLIGHT VIBRATION FELT DURING DESCENT PHASES OF FLT AT HIGH SPEEDS AND DESCENT PITCH ATTITUDES ONLY (HIGHEST AROUND 290 & DECREASES UNTIL NEGLIGABLE BELOW 225KNOTS). VIBRATION SEEMS TO CORRELATE WITH SPEED & SEEMS UNRELATED TO ENGINES/ THRUST. IT ONLY OCCURS Jul 9, 2025 · N591QS · Cessna 680ASDR JJBA20250721062Angle · crackedCRACK ON LH WING TO BODY FAIRING LOWER ANGLE #4 BTW FR 48-49. ON LH WING TO BODY FAIRING LOWER ANGLE #4 BTW FR 48-49 REPAIREDJul 8, 2025 · N11199 · Emb EMB145XRSDR SCNA20250930389Fairing · crackedCRACK SUPPORT OF SETTLEMENT AREA OF PANEL 191AR AT BODY-FAIRING. - RESOLUTION: EMP 283816 - SUPPORT OF SETTLEMENT AREA OF PANEL 191AR AT BODY-FAIRING WAS REPLACED PER B737-800 SRM 51-40-02-0G-0Jul 7, 2025 · N838SY · Boeing 73786NSDR IPXA2025080177856Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT- Z100- STR: RH WTB T-CHORD BETWEEN STA 1037 - STA 1060 RBL 65 HAS EXFOLIATION ON UPPER SURFACE. INSTALLED T-CHORD P/N UP-149N7553-28, BETWEEN STA 1037 - STA 1060 RBL 65IAW B757-200PF, SRM 51-40-02Jul 5, 2025 · N407UP · Boeing 75724APFSDR CALA2025070706267Bracket · corrodedFUSELAGE UPPER AREA IN AREA OF LIVETV FARING/RADOME HAVE S ERVERAL SPOTS OF EVIDENCE OF CORROSION. REPAIR WAS PERFORMED ON FUSELAGE UPPER AREA OF LIVETV FARING RAD OME IAW WORK PER EC/RA #5330-07557 AND EA 757-4434-13- A3968 REV- .Jul 3, 2025 · N41135 · Boeing 757224SDR VNAA20250629032Support · corrodedAFT WING-TO-FUSELAGE FAIRING SUPPORT AT FS 881 LH LOWER ANGLE IS CORRODED. REMOVED DAMAGED LOWER ANGLE OF FAIRING SUPPORT AT FS 881, LH IAW CRJ900 SRM 51-42-006-001-001-A01. LOCATED AND DRILLED AND INSTALLED NEW SH690-39331-7S SUPPORT TO WEB AT FS 881, LH IAJun 29, 2025 · N636NN · Cndair CL6002D24SDR VNAA20250629031Support · corrodedR/H AFT WING-TO-FUSELAGE FAIRING SUPPORT AT FS 881 RH LOWER ANGLE IS CORRODED. REMOVED UNSERVICEABLE ANGLE AND INSTALLED NEW SERVICEABLE R/H F.S. 881 ANGLE SH690-39331-8A IAW CRJ 900 AMM 51-40-11-001-001-A01.Jun 29, 2025 · N636NN · Cndair CL6002D24SDR SWAA2025070186477Fairing · damagedSTRUT 4 FAIRING HAS AN ENLARGED MOUNT HOLE ON TOP AFT SIDE<[01] C/W 25-172-01732Jun 28, 2025 · N268WN · Boeing 7377H4SDR SWAA2025072985845Tail Cone · crackedPERFROM PERMENANT REPAIR TO 1 INCH CRACK ON TOP LEFT SIDE OF TAILCONE. ACCOMPLISHED PERMANENT REPAIR TO 1 INCH CRACK ON TOP LEFT SIDE OF TAILCONE IAW SRM 51-70-05-2R-2.Jun 26, 2025 · N296WN · Boeing 7377H4SDR SWAA2025063085533Panel · delaminatedPANEL 191FL DELAMINATED AT FWD UPPER EDGE. C/W EA 25-153-01706 REF TTG8Q013DJ06Jun 26, 2025 · N8619F · Boeing 7378H4SDR CALA2025062605896Tee Angle · corrodedWING TO BODY AREA, T-CHORD STA900 BTW RBL45 TO LBL45 HAS CORROSION NOTED AND WEAR MARK*91195281-03((EVALUAT ION)) REF:NR128387. REMOVED AND EVALUATED CORROSION ON T-CHORD STA 900 BTW RBL45 TO LBL45 FOUND TO BE OUT OF LIMITS MATERIAL LOSS 50% WAS REPAIRED I AJun 23, 2025 · N41135 · Boeing 757224SDR SWAA2025062383729Radome · crackedCRACK/PUNCHTURE ON RADOME. FO SIDE <[01]. REMOVED AND REPLACED NOSE RADOME IN ACCORDANCE WITH AMM 53-52-00. NO FURTHER ACTION IS REQUIRED.Jun 19, 2025 · N8637A · Boeing 7378H4SDR ABXA20250619132Panel · departedON MAINTENANCE POST FLIGHT INSP, FOUND ON RT WING TO FUSELAGE PANEL MISSING 196CR. MAINTENANCE INSTALLED RT WING TO FUSELAGE PANEL 196CR IAW AMM 20-11-00. AIRCRAFT RETURNED TO SERVICE.Jun 19, 2025 · N1709A · Boeing 767375SDR JJBA20250723087Fairing · corrodedCORROSION FOUND AROUND LH, RH EXTERNAL EMERGENCY LIGHTS ON FWD BODY FAIRING. FWD BODY FAIRING LIGHTS FROM FAIRING PLATE REMOVED, CORROSION REMOVED OUT OF LIMITS. FWD BODY FAIRING PLATE NEW DRILLED. FWD BODY FAIRING PLATE AND LIGHT EMERGENCY INSTALLED.Jun 17, 2025 · N16147 · Emb EMB145XRSDR UIEA2025061300768Tail Cone · dentedREF DMI #194100: PERFORM PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM SECTION.(<P>PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM SECTION WAS ACCOMPLISHED BY OUTSIDE VENDOR SAL AEROSPACE TECHNOLOGIES W/O #400100088. NO FURTHER DEFEJun 11, 2025 · N5179A · Boeing 73783NSDR CALA2025062005773Tee Angle · corrodedWING TO BODY LOWER T-CHORD CORROSION AT STA. 900, 0BL LH AND RH APPROX. 8". ESFR COMPLETED. REMOVED NUTPLATES OF T-CHORD FROM STA 900 IAW B757-200 SRM 51-40 -02, EVALUATED T-CHORD FROM STA 900 BTW LBL8 TO RBL8, FOUND WAS EXFOLIATION THEREFORE IS OUT OF LIMITS Jun 10, 2025 · N29124 · Boeing 757224SDR CALA2025062005771Support · corrodedLWR MID FUSELAGE FR860 TO FR900 LBL 6 FAIR ING SUPPORT HAS CORROSION AS MARKED. ESFR COMPLETED. ADD EMP:V917067 REMOVED CORROSION IAW B757-200 SRM 51-10-02-0G, EVALUATED AREA W ITH FOLLOWING MEASURES: ORIGINAL THICKNESS: 0.080", REMAINING TH ICKNESS: 0.072", TJun 10, 2025 · N29124 · Boeing 757224SDR DALA2025060904396Fairing · delaminatedSHIP 3143 FOUND WING TO BODY PANEL 192AB DELAMINATION ON WALKAROUND. CORRECTIVE ACTION: REMOVED AND REPLACED PANEL 192AB IAW A319 AMM 53-25-11. (7558541).Jun 8, 2025 · N343NB · Airbus A319114SDR SWAA2025071579383Support Angle · crackedCRACK SUPPORT ANGLE ON BODY FAIRING STRUCTURE BS 500D LEVEL STRINGER 19L AT LOWER FUSELAGE. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT WING TO BODY FAIRING STRUCTURE BSTA 500D AT LEVEL OF STRINGER 19L. LOWER FUSELAGE. IAW SRM 51-40-02 . SRM 51-10-02 PARJun 7, 2025 · N292WN · Boeing 7377H4SDR IXXA2025060501Support · corrodedFOUND CORROSION COMMON TO RH FUSELAGE FAIRING PNL 198LR ON SUPPORT STRUCTUREJun 5, 2025 · N754CX · Boeing 7572Y0SDR SWAA2025060978168Panel · debondedPANEL 191D HAS DISBOND ON EXTERIOR SURFACE. REMOVED DAMAGE PER SRM 51-70-05-2R-1. APPLIED REPAIR PER SRM 51-70-05-2R-1. RESIN SEALED REPAIR PER SRM 51-70-08 AND RESTORED PAINT PER AMM 51-21-99.Jun 4, 2025 · N8761L · Boeing 7378SDR SWAA2025061777526Panel · debondedPANEL 193AR INNER SURFACE HAS MULTIPLE DISBONDS. PANEL 193AR WAS REPLACED ON CUSTOMER FAULT TTG8Q010RK8D.Jun 2, 2025 · N298WN · Boeing 7377H4
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