JASC 5350
Service difficulty reports · 6,124
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 ASAA0080138Structure · corrodedPHX - DURING 15K CHECK, THE WING-TO-BODY FAIRING LOWER SUPPORT STRUCTURE WAS FOUND CORRODED AT FS 1000-1013, BL 0 TO RBL 10. REMOVED CORROSION PER SRM 53-01. (M)SDR ASAA0080131Structure · corrodedPHX - DURING 15K CHECK, THE LOWER WING-TO-BODY FAIRING SUPPORT STRUCTURE WAS FOUND CORRODED AT FS 902, RBL 18. REMOVED CORROSION PER SRM 53-01. (M)SDR DHL2000717103Fairing · crackedAT D-CHECK, FAIRING PANEL NR 3334 HAD A CRACK ON THE INSIDE BRACKET MOUNT. CUT OUT DAMAGED AREA, INSTALLED REPAIR AT FAIRING PANEL PER SRM 51-30-2, 8.5 X 2.SDR TWAA0002209Tail Cone · ejectedON THE GROUND, THE TAIL CONE WAS INADVERTANTLY DEPLOYED. REINSTALLED TAIL CONE ASSEMBLY PER MC8-5303. OP16 08-24-97 MCI..SDR QXEA0000596Bracket · crackedPDX - LEFT-HAND BELLY FAIRING HANGER BRACKETS A WING Z STRINGERS 2.24 AND 2.19 ARE CRACKED AT BL 1562L. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01.SDR QXEA0000595Fairing · crackedPDX - LEFT-HAND LOWER WING ROOT FAIRING, INBOARD WALL AT BL 225L TOP CUTOUT FOR Z STRINGER 2.03 CRACKED IN LOWER RADUIS. REPAIRED IAW HORIZON AIR EA 4-53-999.SDR QXEA0000549Fairing · damagedPDX - IN LEFT LOWER WING ROOT FAIRING INBOARD WALL AT BL285L TOP CUT OUT FOR Z STRINGER 2.01 CRACKED IN LOWER RADIUS. REPAIRED IAW HORIZON AIR EA 4-53-999.SDR DHL200080341CFairing · crackedAT C-CHECK, RT WING LOWER SKIN FAIRING SHOWS CRACK 1.25 INCH AT XW 90. FABRICATED DOUBLER IAW SRM 57-2-0 PG 8, INSTALLED DOUBLER IAW SRM 51-1-8 PG 11 AND 12. N/R 1159SDR P2EA00039Skin · dentedSJO - DURING Q-CHECK, LEADING SKIN DENTED ON OUTBOARD FORE FLAP, RIGHT WING. REPAIRED FORE FLAP LEADING EDGE SKIN FROM WBL 414.4 IAW SRM 57-50-4 FIG 1. (M)SDR DHL2000803119Fillet · deterioratedAT C-CHECK, FUSELAGE FILLET DETERIOATED AT FS 660.00 NEAR L-22 RT. REMOVED DETERIOATED FILLET AND REBUILT FILLET ALCLAD 2024-T3 0.032 IAW SRM 53-2-0. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 12. INSTALLED FILLET IAW SRM 53-2-0.SDR DHL200071719DFairing · delaminatedAT D CK, AFT CARGO DOOR SLIDING FAIRING, HAS SEVERAL AREAS OF DELAMINATION, PUNCTURES AND DENTS. INSTALLED FIBERGLASS OVERLAY REPAIRS AS PER SRM 51-40-8, FIG 1, SIZE; 4 BY 4, 10 BY 10 AND 8 BY 8. REF: N/R 3282.SDR AALA006006Warning Light · illuminatedSFO - DURING TAKEOFF AT 60 KNOTS, TAILCONE LIGHT ILLUMINATED AND CAPTAIN ABORTED TAKEOFF. RESET TAILCONE LOCK SWITCH PIN AND LANYARD AND CLEARED UNSAFE ANNUNCIATION. (M)SDR DHL2000803126Fairing · delaminatedAT C-CHECK, RT WING TO FUSELAGE FAIRING NR 709 DELAMINATED AT UPPER SKIN. REMOVED SCREWS AND DELAMINATED PANEL IAW SRM 51-3-0 PAGE 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11 & 12. REPLACED AND SECURED COVER WITH SCREWS IAW SRM 51-3-0 PAGE 1 & 2 (SDR DHL2000803125Fairing · delaminatedAT C-CHECK, LT WING TO FUESLAGE FAIRING NR 705 UPPER SKIN DELAMINATED. REMOVED SCREWS AND DELAMINATED PANEL IAW SRM 51-3-0 PAGE 3. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11&12. INSTALLED OVERHAULED PANEL (WITH SERVICEABLE TAG) AND SECURED WITH SCRESDR DHL2000803124Fairing · delaminatedLEFT WING TO FUSELAGE FAIRING DELAMINATED. REMOVED FASTENERS AND PANEL FOR REPAIR IAW SRM 51-1-21A PAGE 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8 PAGE 11 & 12. INSTALLED OVERHAULED PANEL (WITH SERVICEABLE TAG) AND SECURED CHERRY MAX RIVETS IAW SRM SDR DHL2000803127Fairing · delaminatedAT C-CHECK, LT WING TO FUESLAGE FAIRING NR 704 DELAMINATED AT UPPER SKIN. REMOVED FASTENERS AND DELAMINATED PANEL IAW SRM 51-1-2A PAGE 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11 & 12. INSTALLED OVERHAULED PANEL AND SECURED WITH SOLID RIVETS IAW SSDR MWEA99937Clip · crackedEXTERIOR TAIL CONE RELEASE HANDLE FAILED PULL TEST. AFT CLIP IS CRACKED. MAINTENANCE REMOVED AND REPLACED AFT HANDLE RETATINER CLIP.SDR CALA9901743Fairing Support · corrodedINSPECTION FOUND RT LOWER BODY FAIRING 3441 SUPPORT NR 7 CORRODED AT STA 720F, S26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9901708Skin · corrodedINSPECTION FOUND RT BODY FAIRING 3441 INNER SKIN AND SUPPORT NR 22 CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. THE SUPPORT WAS REMOVED AND A DOUBLER AND BRACKET WERE INSTALLED SDR CALA9901706Skin · corrodedINSPECTION FOUND LEFT LOWER BODY FAIRING 3341 SKIN AND NR 7 SUPPORT CORRODED. THE SKIN WAS REMOVED AND NEW SKIN, DOUBLER, AND STRAPS WERE INSTALLED IAW SRM 53-30-3 AND 51-20-4. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901665Support · corrodedINSPECTION FOUND RT LOWER BODY FAIRING SUPPORT NR 10 CORRODED. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.SDR CALA9901652Latch · out of rigTAIL CONE PULL FROM INSIDE HANDLE WAS EXCESSIVE. THE TAIL CONE WOULD NOT DEPLOY FROM THE AFT SERVICE DOOR. THE TAIL CONE LATCHES WERE ADJUSTED AND OPERATIONAL CHECKS WERE GOOD IAW MM 53-53-00.SDR QXEA9902629Skin · crackedYXX - COMPOSITE TAIL CONE LOWER SKIN CRACKED JUST AFT OF INSPECTION PANEL OPENING, RIGHT OF CENTER. REPAIRED IAW DHC-8 SRM 51-70-00, PAGES 11-19 AND 601.SDR CALA9901560Fairing · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING I/B FLAP FAIRING O/B SIDE PANEL 549AL. A REPAIR WAS INSTALLED IAW SRM 57-00-01.SDR CALA9901508Cables · out of adjustTHE INTERIOR AND EXTERIOR TAIL CONE RELEASE HANDLES REQUIRED EXCESS FORCE TO DEPLOY TAIL CONE. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-01.SDR 99ZZZX4352Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SKIN APPROXIMATELY LBL 20 STA 950F - STA 970.SDR TWAA9917606Fairing · wornDURING OP 16 MAINT CHECK, FOUND RT WING LOWER EDGE OF FAIRING WAS WORN INTO FUSELAGE, STA 813 TO 816, FAIRING NUMBER 2207A. METAL HAD THICKNESS IND OF 0.048 AT STA 813, LONGERON 26R. REMAINDER OF AREA WAS OK. INSTALLED DOUBLER PER SRM 53-04, FIG 53, SHEET 1SDR 2000ZZZX681Fairing · damagedPANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX680Fairing · damagedPANEL 161V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR QXEA9902265Fairing · delaminatedPDX - THERE ARE NUMEROUS DELAMINATED AREAS ON COMPOSITE AERODYNAMIC FAIRING AROUND ACCESS PANEL 261AT. REPAIRED IAW HORIZON AIR EA 9-53-492, STEPS 13-20, AND SRM 51-40-11.SDR 20000505AP022Fairing · crackedNR 5 FLAP TRACK MOVEABLE FAIRING, FORWARD RIB CRACKED AT LOCK BOLT SAFETY WIRE HOLE. INSTALLED REPAIR PER SRM 51-40-3 PAGE 3. (M)SDR RAAA99E9026Radome · damagedDURING APPROACH TO ANC, AIRCRAFT STRUCK BY LIGHTNING. RADOME RECEIVED DAMAGE. REPAIRED PER SRM 53-1-6 NEGLIGIBLE DAMAGE.SDR DHL9974219CFairing · dentedAT C-CHECK, DENT AT WING TO FUSELAGE FAIRING AT APPROX STA 720E ATR 26RT. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 6.5 BY 2.5, N/R 5461.SDR QXEA9902224Fairing · chafedPDX - FUSELAGE HAS CHAFE DAMAGE FROM PANEL 92BD AFT LEFT WING FAIRING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4.SDR QXEA9902223Fairing · chafedPDX - FUSELAGE HAD CHAFE DAMAGE FROM PANEL 91BD AFT RIGHT WING FAIRING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, PARAGRAPH 3C.SDR COMA9960554Radone · bird strikeAFTER DEPARTURE FROM CVG, THE AIRCRAFT ENCOUNTERED A BIRD STRIKE ON NOSE SECTION. AIRCRAFT RETURNED TO THE FIELD. COMPLIED WITH BIRD STRIKE INSPECTION, NO DEFECTS NOTED.SDR 20000522AP026Fairing · crackedFOUND DURING D-CHECK, D PIT AFT DOOR FRAME FAIRING CRACKED. REMOVED FAIRING. FABRICATED FAIRING IAW DC-8 SRM 51-1-4. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3-0. (M)SDR 20000427AP003Fairing · crackedFOUND DURING D-CHECK, D PIT FORWARD DOOR FRAME, FAIRING CRACKED. REMOVED FAIRING. FABRICATED FAIRING IAW DC-8 SRM 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3-0. (M)SDR USAASB99238Fairing · missingBOS - FLT 8053 - FLIGHT RETURNED TO FIELD AT BOS DUE TO A LOUD HIGH PITCH HUMMING NOISE AND VIBRATION AROUND CABIN WINDOW AT SEAT ROW 9ABC. VIBRATION AND HUMMING NOISE DECREASED UNDER 10,000 FT AND 220 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENASDR UPS99530675Radome · damagedINSPECTION TYPE:N/A, PILOT REPORT, RADOME DAMAGED FROM BIRD STRIKE EXCEEDS LIMITS. REMOVED AND REPLACED RADOME PER MM 53-12-01 PAGE 201 (P/N 4910-400), (S/N 393NF) ON, (P/N 121N 7820-12), (S/N 150) OFF.SDR CALA9901266Fairing · crackedINSPECTION FOUND A 3 INCH CRACK IN RT HORIZONTAL STABILIZER FAIRING. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.SDR EIA990276Fillet · crackedMZJ - DURING C-CHECK, ELONGATED HOLES AND CRACKS WERE FOUND ON THE UPPER LEFT WING TO FUSELAGE FILLET. REPAIRED BY TRIMMING ELONGATED HOLES, FABRICATED AND INSTALLED REPAIR DOUBLER PER ECRA 932-53-049-2. (M)SDR USAA991010Fairing · crackedCMH/PIT - CMH LINE MAINTENANCE FOUND 10 INCH CRACK AT UPPER RIGHT FUSELAGE TOWING FAIRING STATION 714. INSTALLED EXTERNAL DOUBLER PER EA 52894 AND SRM 53-40-02. (M)SDR DHL9972738CFairing · delamiantedAT C CHECK, LWR LT BODY FAIRING AFT OF HYD ACCESS PANEL 3519 DELAMINATED AT LWR I/B END AND ALONG EDGE. ALSO, MISSING TWO FASTENERS. REMOVED LWR LT BODY FAIRING PER SRM 51-30-2, REPLACED MISSING FASTENERS PER SRM 51-30-2, INSTALLED FG OVERLAY REPAIR AS PER SSDR 99ZZZX3501Fairing · wrinkledDURING LANDING, LEFT WING TIP TANK CONTACTED THE RUNWAY. BOTTOM OF TIP TANK DENTED AND SCRAPED. LEFT WING TO FUSELAGE UPPER FAIRING WRINKLED. LEFT SIDE OF FUSELAGE ABOVE AFT END OF INBOARD FAIRING SLIGHTLY WRINKLED. EXACT CAUSE YET TO BE DETERMINED, BUT APSDR CALA9901116Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RIB AT LT INNER CAVITY OF TAIL CONE. THE RIB WAS TRIMMED OUT AND THE AREA WAS REINFORCED WITH AN ANGLE REPAIR IAW SRM 53-00-00, FIGURE 1 AND 51-31-01.SDR CALA9901115Spar · shearedINSPECTION FOUND THE TAIL CONE WORK PLATFORM SPAR SHEARED IN SEVERAL PLACES. THE SHEARED AREAS WERE TRIMMED OUT AND REINFORCED WITH DOUBLERS IAW SRM 53-00-01, FIGURE 4 AND 51-31-01.SDR 99FDEA00365Fillet · missingPIECE OF AC LOST ON T/O ROTATION. LEFT SLAT TO FUSELAGE FILLET DEPARTED A/C. INSP FUSELAGE AFT OF MISSING PERFORMANCE FAIRING NO DAMAGE NOTED. ALSO INSPECTED NR 2 ENG INTAKE WITH NO DAMAGE NOTED. REMOVED AND REPLACED CLOSE-OUT STRIP OF I/B 1L SLAT UPON INSSDR UF6A990814Fairing · crackedSBN - LEFT HORIZONTAL FAIRING ATTACHMENT TO FUSELAGE IS CRACKED. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW ENGINEERING REPORT NR 99-153. (M)SDR UF6A990813Fairing · crackedSBN - RIGHT VERTICAL FAIRING ATTACHMENT TO FUSELAGE IS CRACKED. MAINTENANCE REPAIRED CRACKED. ALL WORK WAS DONE IAW ENGINEERING REPORT NR 99-153. (M)
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