JASC 5350

Service difficulty reports · 6,105

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 SWAA2026101639244Radome · crackedRADOME CRACKED AT 6 OCLOCK POSITION, R & R THE NOSE RADOME IAW AMM 53-52-00.Oct 12, 2026 · N486WN · Boeing 7377H4SDR DALA2026100905577Tail Cone · puncturedTAIL CONE DECAL DAMAGED & PUNCTURED, REPLACED THE DECAL IAW MM 52-20. (9388108) (AIRCRAFT GROUNDED).Oct 8, 2026 · N921AT · Boeing 717200SDR IPXA2026100957455Radome · brokenBROKEN COMPOSITE , RADOME EXTERNAL 2 AREA. IAW EO-35385-JIC001, REV 4, INSTALL RADOME BOOT. CONDITION CHECKED SATISFACTORY.Oct 2, 2026 · N364UP · Boeing 767346SDR R61A2026092700285Strap · corrodedWHILE AC WAS IN FOR HVY CK FOUND CORRODED FWD WTB FAIRING TO FUSELAGE STRAP FOUND ON CF1 AT FR 27-28 , S28L-S24R. MX REPLACED STRAP IAW SRM 51-42-02, 51-43-04 AND 51-41-02.Sep 27, 2026 · N211JQ · Emb ERJ170200LRSDR SWAA2026100529699Radome · delaminatedNOSE RADOME HAS DELAMINATION. NOSE RADOME REPLACED ON TTG8Q01ES0U2.Sep 22, 2026 · N8888M · Boeing 7378SDR DALA2026092205299Radome · damagedBIRD STRIKE ON RADOME ON APPROACH NO UNUSUAL INDICATION OR SMELL FOLLOWING STRIKE. C/W BIRD STRIKE INSPECTION IAW AMM 05-51-14. NO OTHER DAMAGE NOTED. STRIKE ON RADOME DEFERRED TO MON WITH COMPLETIOIN OF ERA 637070-14 REV ORIGINAL. SEC 1. PERMINENT REPAIR WITSep 20, 2026 · N369NW · Airbus A320212SDR CALA2026092119620Bracket · corrodedRIGHT LWR WING TO BODY FAIRING, BY THE RAM AIR INLET AT BS 880 RBL 20, ONE BRACKET CORRODED. THE BRACKET WAS REMOVED AND REPLACED AND LID WAS REMOVED AND REPLACED IAW DWG 149N7160, REV K IAW SRM 51-40-05-0G, AND SRM 51-40-05-0G.Sep 18, 2026 · N18112 · Boeing 757224SDR DALA2026092105251Radome · damagedBIRD STRIKE ON JACCC SID NEAR L IDAS AT APPROX 6000 FT. NOSE OF A/C. CLEANED LOWER PART OF THE RADOME WHERE BIRD STRUCK. PERFORMED INSPECTION OF THE AIRCRAFT AFTER A BIRD STRIKE PER A320 AMM TASK 05-51-14-200-803-A, FOUND INTERNAL DISBONDING/DELAMINATION AND Sep 18, 2026 · N375NC · Airbus A320212SDR IPXA2026092267592Fairing · debondedDEBONDED SKIN , RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. BOND THE FOIL WITH RESIN CURED AT 200°F FOR 220 MINUTES Sep 16, 2026 · N355UP · Boeing 76734AFSDR N6WA2026091803Support Frame · corrodedFRAME SUPPORT STRUCTURE RT AFT FAIRING AT FS 939 IS OUT OF LIMITS. REMOVED AND REPLACED RT FRAME SUPPORT STRUCTURE AFT FAIRING AT FS 939 IAW SRM 51-26-00.Sep 16, 2026 · N526GJ · Cndair CL6002C11SDR SWAA2026101493635Access Panel · delaminatedDELAMINATED ACCESS PANEL 194CR ON BODY FAIRING. REPAIRED THE ACCESS PANEL ON THE BODY FAIRING IAW SRM 51-70-04-2R-2, REPAIR 2.Sep 15, 2026 · N8656B · Boeing 7378H4SDR DALA2026091805226Angle · crackedCRACK ON ANGLES ON WING TO BODY FAIRING STRUCTURE. BS 1180+60, S26R. REPAIRED PER B757-300 SRM 51-70-11 (1813690)(AIRCRAFT GROUNDED)Sep 15, 2026 · N595NW · Boeing 757351SDR SWAA2026091677980Tail Cone · delaminatedDELAMINATION ON TAIL CONE AT 4 O'CLOCK. REMOVED DAMAGED SKIN IAW SRM.53-80-70-2R-1, REPAIR 1, 51-70-05-2R-11, REPAIR 11, SRM 51-70-05-2R-1, REPAIR 1. APPLIED POTTING & CURED IAW SRM.51-70-05-2R-11, REPAIR 11. APPLIED HOT BOND REPAIR TAP TEST FAILED IAW SRM.5Sep 15, 2026 · N7889A · Boeing 73779LSDR DALA2026091505150Support · corrodedCORROSION ON WTB FAIRING SUPPORT STRUCTURE BETWEEN FRAME 43 AND FRAME 44 AT STR 36R. C/W ER/A 636701-14 REV ORIGINAL. (LP# 1813148; AIRCRAFT WAS GROUNDED).Sep 14, 2026 · N139DU · Airbus BD5001A10SDR DALA2026091505143Access Panel · corrodedLEVEL 2 CORROSION, APU EXHAUST TAIL CONE AT FR 86, ACCESS PANEL 317AL WERE FOUND FRAME AUXILIARY, TRANSFORMER REAR NAVIGATION LIGHT AND BONDING ANGLE WITH CORROSION AND AT FUSELAGE AREA FOUND FR 86 LOWER FRAME SECTION (CHANNEL) WITH CORROSION. (LP: 1813002, AISep 14, 2026 · N345NB · Airbus A319114SDR 2026FA0000692Radome · abnormalWHILE TAKING DELIVERY OF A NEW AIRCRAFT, NOTICED THE RADOME TO FUSELAGE CONTOUR HAS A MISMATCH. THE RADOME IS BIGGER THAN THE FUSELAGE. AT THE SAME TIME TEXTRON WAS DELIVERING S/N 525B-0917 AND IT HAD A LARGER MISMATCH. WAS TOLD BY TEXTRON REPRESENTATIVES THSep 14, 2026 · N765JW · Cessna 525BSDR DXTA2026091509690Sealant · misinstalledDURING DESCENT FROM AROUND FL200 A LOW LOUD HUM STARTED. WE WERE AROUND 295-300KTS VIBRATION FELT IN FEET FROM LEFT AND RIGHT PILOT. WORSE VIBRATION FELT FROM THE FLOOR INLINE WITH THE MAIN CABIN DOOR. VIBRATION AND SOUND STOPPED AT 11,000FT IN LEVEL OFF AFTERSep 13, 2026 · N444QS · Emb EMB505SDR VNAA2026091102Angle · corrodedON AFT WING TO FUSELAGE FAIRING SUPORT STRUCTURE FOUND LT ANGLE BS 939, RT ANGLE BS 939 & ANGLE ARE CORRODED. REFERENCE SRM 53-82-55-001-002-A01 SHEET 5 OF 5 ITEMS 96, 97 AND 98). REMOVED AND REPLACED CORRODED ANGLES.Sep 11, 2026 · N507AE · Cndair CL6002C10SDR DALA2026091605180Longeron · corrodedCNTR WING TO BODY FAIRING LONGERON, BTWN FR46 AND FR48, RBL 9, BTWN FR48 AND FR52, LBL 5, CORRODED TIME LIMITED. ACCOMPLISH REPETITIVE INSPECTION PER ERA 636699-14 EVERY 1000 FH AND TERMINATING ACTION WITHIN 10,000 FH FROM 9 SEP 2026. ASSOCIATED ER/A 00-6366Sep 9, 2026 · N139DU · Airbus BD5001A10SDR DALA2026091605178Longeron · corrodedFUSELAGE, WTB FAIRING LONGERON, BETWEEN FR 48 - 52, RBL 5. CORROSION TIME LIMITED REPAIR. INSPECT THE SUBJECT AREA IAW ERA 636701-14, SEC II, EVERY 1000 FH AND TERMINATING ACTION DUE WITHIN 10,000 FH FROM REPAIR ACCOMPLISHMENT, DTE STAGE III. ASSOCIATED ER/A Sep 9, 2026 · N139DU · Airbus BD5001A10SDR DALA2026091105090Support · corrodedCORROSION ON WTB FAIRING SUPPORT STRUCTURE AT LONGERON 20" AFT OF FR48 TO FR52 LBL4. ACCOMPLISHED ER/A# 636699-14 REV-ORIGINAL. ASSOCIATED ER/A 14-636699 ADDED FOR AC 8139. (LP# 1804346; AIRCRAFT WAS GROUNDED)Sep 9, 2026 · N139DU · Airbus BD5001A10SDR DALA2026091105089Support · corrodedCORROSION ON WTB FAIRING SUPPORT STRUCTURE FROM FRAME 46R TO FRAME 46R+4" AT STR 35R. . ACCOMPLISHED ER/A# 636699-14 REV-ORIGINAL. ASSOCIATED ER/A 14-636699 ADDED FOR AC 8139. (LP# 1804322; AIRCRAFT WAS GROUNDED)Sep 9, 2026 · N139DU · Airbus BD5001A10SDR HNAA2026100100935Angle · crackedRIGHT FR48, WING STUB, WING TO BODY, ANGLE CRACKED. R & R ANGLE IAW SRM 51-40-02Sep 8, 2026 · N650AE · Emb EMB145LRSDR 1Q2R2026092020076Diaphragm · crackedLEFT LOWER WING-TO-FUSELAGE FAIRING AT FS909.00 DIAPHRAGM IS CRACKED 1.60" FROM LOWER T/E. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130787 REV. 0, DATED SEPTEMBER 08, 2026, AND MHI RJ REO 670-53-82-478 REV. -A, DATED NOVEMBER 12, 2014.Sep 8, 2026 · N706PS · Cndair CL6002C10SDR DALA2026091605181Longeron · corrodedER/A 636601-14 CORROSION REPAIR TO WING TO BODY FAIRING LH LONGERON BETWEEN FR 40 TO FR 48 REQUIRES FOLLOW ON ACTION. ACCOMPLISH 636601-14 SECT II REP INSPECTION WITHIN EVERY 1000 FLIGHT HOURS FROM SECT I ACCOMPLISHMENT. ACCOMPLISH SECT III PERMANENT REPAIR WISep 8, 2026 · N301DU · Airbus BD5001A11SDR EE4Y2026090824946Rib · crackedDURING THE INSPECTION, WAS FOUND IN THE LT WING TO FUSELAGE FAIRING AT FR52 THE RIB CRACKED, DUE TO THIS, WAS PERFORMED A PERMANENT REPAIR IAW ETD2016-190-054721 DTD JUN 10 2016 AND DOCUMENTED UNDER COOPESA EO # COO-EO-2026-24815-R00 DTD AUG 03 2026. JOB A1Q35Sep 8, 2026 · N306JB · Emb ERJ190100IGWSDR 1Q2R2026092220197Diaphragm · crackedLEFT LOWER WING-TO-FUSELAGE FAIRING AT BS 909 DIAPHRAGM IS CRACKED, 1.60" FROM LOWER T/E. PERFORMED PERMANENT REPAIR IAW RFTS-130820 REV. 0, AND REO 670-53-82-478 REV. -A.Sep 7, 2026 · N528EG · Cndair CL6002C10SDR IPXA2026091123185Fairing · erodedERODED PANEL , WING TO BODY FAIRING PANEL 192AR FWD EDGE. I.A.W. 747-8F SRM 53-00-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-80-03-0G-0 REV. 49 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE EROSION MATERIALS AND CLEAN.1.2 MEASURE THE DAMAGE AREA ( L : 7", W Sep 7, 2026 · N623UP · Boeing 7478FSDR IPXA2026091223189Panel · erodedEROSION - PANEL, WING TO BODY FAIRING PANEL 192AGR FWD EDGE. IAW SRM 53-00-70-2R-1 REFER TO SRM 51-70-05-2R-1 AND SRM 51-80-03-0G-0 REV. 49 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE EROSION MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE AREA ( L : 14", W : 1.2Sep 7, 2026 · N623UP · Boeing 7478FSDR IPXA2026091223226Panel · erodedERODED PANEL, WING TO BODY FAIRING PANEL 191FFL FWD EDGE. I.A.W. 747-8F SRM 53-00-70-2R-1 REFER TO SRM 51-70-05-2R-1 AND SRM 51-80-03-0G-0 REV. 49 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE EROSION MATERIALS AND CLEAN.1.2 MEASURE THE DAMAGE AREA ( L : 5.5",Sep 7, 2026 · N623UP · Boeing 7478FSDR SWAA2026101461993Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL, WING TO BODY FAIRING. REPAIRED THE W-B FAIRING ACCESS PANEL 193CL IAW SRM 51-70-05-2R-10, REPAIR 10.Sep 4, 2026 · N8656B · Boeing 7378H4SDR CALA2026090319212Panel · damagedFAIRING PANEL 192DT RAMP DISCOVERED PANEL 192 DT DAMAGED ON WALK AROUND. NO LARGE PORTIONS OF PANEL DEPARTED AIRCRAFT. PANEL WAS TORN FROM LEADING EDGE AROUND 2 FT TOWARD THE BACK.Sep 2, 2026 · N831UA · Airbus A319131SDR UIEA2026082700808Support Frame · brokenBS 1480, RT BLG WW FIXED FAIRING SUPPORT FRAME FOUND BROKEN. THE SUPPORT FRAME WAS REPAIRED IAW RI-53-60-18459, REV A. NO FURTHER DEFECTS NOTED.Sep 1, 2026 · N489MC · Boeing 747412FSDR SWAA2026100589554Access Panel · delaminatedDELAMINATED WING TO BODY FAIRING ACCESS PANEL 193CL. REPAIRED THE ACCESS PANEL 193CL IAW SRM 51-70-05-2R-10, REPAIR 10.Aug 30, 2026 · N8712L · Boeing 7378SDR DALA2026083104911Switch · looseTAIL CONE EXIT TOGGLE SWITCH/LATCH LOOSE. CORRECTIVE ACTION: RESECURED AND ADJUSTED HARDWARE PER B717 AMM 52-22, NO OHTER FAULTS NOTED A/C OK TO CONT IN SVC. (9488400) AIRCRAFT WAS GROUNDED.Aug 30, 2026 · N928AT · Boeing 717200SDR DALA2026090104932Frame · corrodedCORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783796; AIRCRAFT WAS GROUNDED)Aug 29, 2026 · N301DU · Airbus BD5001A11SDR DALA2026090104931Frame · corrodedCORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783791; AIRCRAFT WAS GROUNDED)Aug 29, 2026 · N301DU · Airbus BD5001A11SDR CALA2026090119118Support Frame · crackedLEFT WING TO BODY FAIRING SUPPORT FRAME CRACKED. REPAIRED THE WING TO BODY SUPPORT FRAME IAW REO G26037 AND EC/RA 5360-02207, REV -.Aug 29, 2026 · N23707 · Boeing 737724SDR HNAA2026100500947Angle · crackedRIGHT WING STUB, FUSE TO WING BOX ANGLE CRACKED AT FR 46. R & R ANGLE IAW SRM 51-40-02Aug 27, 2026 · N653AE · Emb EMB145LRSDR R61A2026092600273Strap · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND AFT WTF FAIRING ATTACHMENT STRAP BETWEEN FR 73- 75, STR 23R - 29R CORRODED. THE ATTACHMENT STRAP WAS REMOVED AND REPLACED IAW SRM 51-43-04 AND 51-41-02.Aug 27, 2026 · N211YX · Emb ERJ170200LRSDR 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.Aug 27, 2026 · N211YX · Emb ERJ170200LRSDR 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.Aug 27, 2026 · N211YX · Emb ERJ170200LRSDR 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.Aug 26, 2026 · N211YX · Emb ERJ170200LRSDR SWAA2026090169727Panel · delaminatedPANEL 193CL LEADING EDGE HAS AREA OF EROSION AND DELAMINATION. R & R PANEL 193CL PER AMM 53-51-21.Aug 25, 2026 · N8546V · Boeing 7378H4SDR 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)Aug 24, 2026 · N314NB · Airbus A319114SDR 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.Aug 20, 2026 · N266WN · Boeing 7377H4SDR 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.Aug 19, 2026 · N33292 · Boeing 737824SDR 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.Aug 19, 2026 · N33292 · Boeing 737824SDR SWAA2026092873584Panel · debondedPANEL 192BR OUTER SKIN IS DISBONDED NEAR THE FWD EDGE. THE PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.Aug 18, 2026 · N8643A · Boeing 7378H4SDR 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-Aug 16, 2026 · N372UP · Boeing 767300
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