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.

SDR EIAA970195Fairing · crackedSYD - LOG PAGE: F27377 - WING TO BODY FAIRING DAMAGED BEHIND LT BODY GEAR FROM NR 8 TIRE TREAD SEPARATION. TEMP REPAIRED PER SRM 51-40-16, PERMANENT REPAIR NEXT SCHEDULED A-CHECK. REF: OPERATION CONTROL NR 97ZZZX4780 AND 97ZZZX4781. (X)Sep 8, 1997 · N482EV · Boeing 747212BSDR CALA9701351Release Mech · out of adjustEXCESSIVE PULL WAS REQUIRED TO RELEASE TAILCONE USING THE INTERIOR AND EXTERIOR TAILCONE RELEASE HANDLES. THE TAILCONE RELEASE MECHANISM WAS ADJUSTED IAW MM 53-53-00.Sep 8, 1997 · N16802 · Doug DC982SDR CALA9701350Grommet · looseTHE AFT CABIN DOOR PULL TO RELEASE TAILCONE WAS HIGH. MAINTENANCE FOUND CABLE GROMMET LOOSE CAUSING CABLE TO BIND. THE RUBBER CABLE GROMMET WAS SECURED IAW MM 53-53-00.Sep 8, 1997 · N16802 · Doug DC982SDR CALA9701349Flange · warpedTHE TAILCONE DID NOT RELEASE DURING DROP TEST. MAINTENANCE FOUND THE TAILCONE RING FLANGE WARPED. THE TAILCONE WAS REMOVED AND REPLACED AND THE LATCHING MECHANISM WAS ADJUSTED IAW MM 53-53-00.Sep 8, 1997 · N16802 · Doug DC982SDR 97ZZZX4781Fairing · crackedSYD - LOG PAGE: F27377 - WING TO BODY FAIRING DAMAGED BEHIND LT BODY GEAR FROM NR 8 TIRE TREAD SEPARATION. TEMP REPAIRED PER SRM 51-40-16, PERMANENT REPAIR NEXT SCHEDULED A-CHECK. REF: OPERATION CONROL NR EIAA970195 AND 97ZZZX4782.Sep 8, 1997 · N482EV · Boeing 747212BSDR 97ZZZX4780Fairing · crackedSYD - LOG PAGE: F27377 - WING TO BODY FAIRING DAMAGED BEHIND LT BODY GEAR FROM NR 8 TIRE TREAD SEPARATION. TEMP REPAIRED PER SRM 51-40-16, PERMANENT REPAIR NEXT SCHEDULED A-CHECK. REF: OPERATION CONTROL NR EIAA970195 AND 97ZZZX4781.Sep 8, 1997 · N482EV · Boeing 747212BSDR 97ZZZX3969Radome · departedDURING THE FIRST TEST FLIGHT OF THE NEW BELLY RADOME FOR TIER II: WHILE IN A HIGH SPEED DESCENT OUT OVER THE OCEAN, THE RADOME DEPARTED THE AIRCRAFT. THE AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION INTO THE INCIDENT REVEALED THAT A SHOCK WAVE FORMED ON Aug 28, 1997 · N575HA · Doug EA3BSDR 97ZZZM982Seal · failedWEATHER RADAR (P/N 6228439003) BECAME INOPERATIVE DUE TO EXCESSIVE MOISTURE IN RADOME. EXCESSIVE MOISTURE DUE TO THE RADOME SEAL.Aug 17, 1997 · N844CA · Beech 1900DSDR QXEA9700697Fairing · deterioratedPDX - LEFT-HAND TAIL CONE FAIRING DETERIORATED. REPAIRED IAW EA 4-53-220.Aug 12, 1997 · N490US · Fokker F28MK4000SDR EIAA970188Fairing · crackedYSSY - WING TO BODY FAIRING DAMAGED BEHIND RIGHT BODY GEAR FROM NR 5 TIRE TREAD SEPARATION. REPAIRED AS PER SRM 53-50-02. PERMANENT REPAIR NEXT A CHECK 8/18/97. (M)Aug 10, 1997 · N471EV · Boeing 747273CSDR ASAA9780174Clamp · brokenSEA - DURING TAIL CONE EMERGENCY RELEASE CHECK FROM THE AFT CABIN ENTRY DOOR POSITION, THE TAIL CONE FAILED TO RELEASE. REPLACED BROKEN ADEL CLAMP ON TAIL CONE RELEASE CABLE AND TAIL CONE RELEASED NORMALLY. (M)Aug 10, 1997 · N963AS · Doug DC983SDR 97ZZZM938Fairing · crackedYSSY - WING TO BODY FAIRING DAMAGED BEHIND RIGHT BODY GEAR FROM NR 5 TIRE TREAD SEPARATION. REPAIRED AS PER SRM 53-50-02. PERMANENT REPAIR NEXT A CHECK 8/18/97. (M)Aug 10, 1997 · N471EV · Boeing 747273CSDR P5CA9701398Radome Boot · erodedRADOME BOOT ERODED/PAINT REQUIRES UPGRADE. REPAIRED AND REPLACED UPGRADE PAINT AS REQUIRED PER BOEING SRM 51-24-11, MM 53-52-01.Aug 9, 1997 · N859FT · Boeing 747123SDR WTAA970151Radome · bird strikeSMX - BIRD STRIKE ON LOWER SIDE OF NOSE LANDING REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Aug 7, 1997 · N427UE · Bag JETSTM3101SDR DL73K971518Radome · bird strikeBIRD STRIKE ON LEFT SIDE OF A/C. NO ABNOMAL FLIGHT CHARACTERISTICS OR ENGINE INDICATIONS. AIR TURNBACK, PERFORMED BIRD STRIKE INSP AND NO DAMAGE FOUND. CONFIRMED NO INGESTION INTO ENGINES, ALL LE DEVICES CK NORMAL.Aug 1, 1997 · N324DL · Boeing 737232SDR AALA971386Lights · inoperativeMIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE OF FIRST CLASS CABIN INOPERATIVE. ACCOMPLISHED EMERGENCY FLOOR LIGHT OPERATIONAL CHECK AND ALL FLOOR LIGHTS IN FIRST CLASS AND MAIN CABIN OPERATED NORMALLY. (M)Jul 28, 1997 · N1755 · Doug MD11SDR DLM88971468Tail Cone · damagedTAIL CONE DEPLOYED. REPAIRED TAIL CONE DAMAGE PER ERA 362367-14. REINSTALLED TAIL CONE ESCAPE SLIDE DID NOT DEPLOY BECAUSE PREV HYD LEAK SOAKED VELCRO HOLDDOWN FOR LANDYARD NOT ALLOWING FOLLOW-UP OF SAME TO PULL SLIDE CVR OFF SLIDE. CLEANED VELCRO AND RESECJul 27, 1997 · N931DL · Doug MD88SDR P5CA9701307Radome · delaminatedNOSE RADOME HAS SEVERAL AREAS OF EXPOSED COMPOSITE AND DELAMINATION. CLEANED, SANDED AND POTTED DAMAGED AREA IAW BOEING SRM 53-50-03 AND PREP AND PAINTED SPOTS ON NOSE RADOME IAW 51-24-11.Jul 23, 1997 · N851FT · Boeing 747122SDR UPS97223993Tail Cone · delaminatedINSPECTION TYPE:C AREA OF DELAMINATION LEFT AFT SIDE OF TAIL CONE REPLACMENT CONE FITTED IAW MM 55-30-21Jul 20, 1997 · N923UP · Boeing 72731CSDR WRLA97048Tailcone · damagedDURING PERFORMANCE OF 'A' CHECK, REPAIR AGENCY PERSONNEL ATTEMPTED TO LOWER TAILCONE WHILE UPPER SAFETY HOOKS WERE STILL ENGAGED. ACTION DAMAGED TAILCONE ACTUATOR ATTACH POINT. REPAIR AGENCY MAINTENANCE PERSONNEL PERFORMED REPAIRS TO TAILCONE ATTACH POINT PEJul 6, 1997 · N280WA · Doug MD11SDR 9713319308Release Mech · out of adjustDURING TAIL CONE FUNCTION CHECK, FOUND THAT THE TAIL CONE FAILED TO DROP USING THE AFT EMERGENCY DOOR HANDLE. ALSO, FOUND TAIL CONE RELEASE MECHANISM ARM AT PASSENGER AFT ENTRANCE DOOR CHAFED DUE TO CONTACT WITH DOOR STOP FITTING AND TAIL CONE UPPER LEFT ATTAJul 3, 1997 · N311RC · Doug DC982SDR P5CA9701282Fairing · delaminatedDELAMINATION ON RIGHT AFT FAIRING PANEL 194FR. REPAIRED PER BAC SRM 51-40-09.Jun 30, 1997 · N850FT · Boeing 747122SDR CALA9701113Clips · out of adjustTHE TAILCONE INTERIOR HANDLE PULLED FROM CLIPS AT 37 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.Jun 30, 1997 · N937MC · Doug DC982SDR CALA9701112Cables · out of adjustTHE TAILCONE INTERIOR RELEASE HANDLE REQUIRED 45 POUNDS OF PULL TO RELEASE TAILCONE. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-53-00.Jun 30, 1997 · N937MC · Doug DC982SDR 9712579936Release Mech · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. RIGGED TAIL CONE RELEASE SYSTEM, FUNCTIONAL CHECK OK.Jun 26, 1997 · N1799U · Doug DC931SDR 9712009920Latch Mech · malfunctionedDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ALSO, FOUND 13 WORN ALIGNMENT RECEPTACLES AND LEFT LOWER LATCH DOES NOT OPERATE PROPERLY. REPLACED ALIGNMENT RECEPTACLES, LATCH ASSEMBLY, AND RIGGED RELEASE SYSTEM.Jun 19, 1997 · N972N · Doug DC932SDR QXEA9700461Fairing · chafedAFT FUSELAGE BELLY FAIRING PANEL 91BC HAS CHAFED INTO THE FUSELAGE SKIN ALONG ITS TRAILING EDGE. REMOVED PAINT AROUND AREA, BLENDED AREA AS REQUIRED. NDT INSPECTION SHOWED NO CRACKS. WORK PERFORMED PER EA 4-53-181.Jun 16, 1997 · N493US · Fokker F28MK4000SDR AU970776Fairing · cracked(AUS) CONNECTING FAIRING CRACKEDJun 13, 1997 · Aerosp SA365CSDR ORJA9782Release Mech · out of adjustTAILCONE DID NOT RELEASE WITH EMERGENCY DOOR HANDLE ON AFT ENTRY DOOR. RIGGED TAILCONE EMERGENCY RELEASE SYSTEM PER MM 25-65-00. (M)Jun 5, 1997 · N824RA · Doug DC982SDR P5CA9700557Fairing · delaminatedRIGHT BODY FAIRING AT BS 1000 BY CENTER WING SUMP PLUG PANEL DELAMINATED. REPAIRED PER BOEING SRM 51-40-07.May 29, 1997 · N856FT · Boeing 747132SDR 9710389960Cable · rustedDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ALSO, FOUND LEFT SIDE RELEASE CABLE RUSTED AT UPPER PULLEY. REPLACED CABLE, UPPER LEFT LATCH ASSEMBLY AND LUBED ALL LATCHES, FUNCTIONAL TEST OK.May 28, 1997 · N920RW · Doug DC931SDR 9710379607Latch Mech · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. LUBRICATED LATCH PINS, REPLACED CABLES, AND RIGGED SYSTEM, FUNCTIONAL CHECK OK.May 28, 1997 · N607NW · Doug DC932SDR P5CA9701167Fairing · crackedFX - BODY FAIRING 193F FOUND CRACKED. FIBERGLASS REPAIR PER BOEING SRM 51-40-14, FIG 9.May 26, 1997 · N855FT · Boeing 747124SDR CALA9700826Cables · out of adjustTHE FORCE REQUIRED TO PULL THE TAILCONE INTERIOR AND EXTERIOR RELEASE HANDLES EXCEEDED LIMITS. ADJUSTED TAILCONE CABLES IAW MM 53-53-00.May 26, 1997 · N72824 · Doug DC982SDR P5CA9700850Fairing · delaminatedRT REAR W/W CUTOUT SLOPE FAIRING DAMAGED AND DEFORMED. SMOOTHED OUT SLOPE FAIRING PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-01 AND REFORMED PER SRM 51-40-00.May 24, 1997 · N855FT · Boeing 747124SDR CALA9700808Fillet · missingINSPECTION FOUND THAT A PORTION OF THE LT WING UPPER FILLET FAIRING WAS MISSING DURING A WALKAROUND AFTER AIRCRAFT ARRIVED IN FRA. INSPECTION OF THE AIRCRAFT REVEALED THE ATTACH SCREWS HAD PULLED THROUGH THE FIBERGLASS PANEL (FILLET) AND THE ATTACH SCREWS WERMay 23, 1997 · N14075 · Doug DC1030SDR P5CA9701159Fairing · corrodedLEVEL 1 - FX - BODY FAIRING 191F EXT SKIN FOUND SURFACE CORRODED. REMOVED CORROSION AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.May 21, 1997 · N855FT · Boeing 747124SDR P5CA9701158Fairing · brokenFX - BODY FAIRING 1920 FWD UPPER CORNER FOUND BROKEN. FIBERGLASS REPAIR PER BOEING SRM 51-40-15, FIG 7.May 21, 1997 · N855FT · Boeing 747124SDR P5CA9701157Fairing · crackedFX - BODY FAIRING 291B EXT SKIN PREVIOUS REPAIRED AREA FOUND CRACKED. FIBERGLASS REPAIR PER BOEING SRM 51-40-15, FIG 7.May 21, 1997 · N855FT · Boeing 747124SDR 9710069609Release Mech · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAIL CONE. RIGGED TAIL CONE RELEASE SYSTEM, FUNCTIONALLY CHECKED OK.May 20, 1997 · N609NW · Doug DC932SDR 9710059763Clips · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR RELEASE HANDLE FROM THE RETAINING CLIPS. ALSO, FOUND THAT 6 ALIGNMENT PINS BOTTOM OUT. SHIMMED ALIGNMENT PINS AND ADJUSTED CLIPS, FUNCTIONAL CHECK OK.May 20, 1997 · N763NW · Doug DC941SDR 9709609310Striker · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT THE TAILCONE DID NOT RELEASE USING THE AFT CABIN EXIT DOOR HANDLE. ALSO, FOUND EXTERIOR RELEASE HANDLE AND SOCKET WORN. REPLACED HANDLE, SOCKET, AND CABLE. ADJUSTED RELEASE ARM STRIKER ON AFT DOOR. OPERATIONAL CMay 15, 1997 · N313RC · Doug DC982SDR WTAA970083Radome · bird strikeSFO - BIRD STRIKE AT RADOME AREA REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)May 13, 1997 · N282UE · Emb EMB120RTSDR CALA9700810Clip · brokenTHE EXTERIOR TAIL CONE RELEASE HANDLE PULLED OUT OF CLIPS AT TEN POUNDS AND 80 POUNDS WAS REQUIRED TO RELEASE TAIL CONE USING EXTERIOR HANDLE. A BROKEN CLIP ON RELEASE HANDLE WAS REPLACED, TIMING BLOCKS WERE ADJUSTED, AND TAIL CONE LATCHES WERE LUBRICATED.May 13, 1997 · N33506 · Doug DC932SDR 9709419972Clips · out of adjustDURING M-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL EXTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. ALSO, FOUND THE LEFT TAIL CONE CABLE FRAYED BELOW TOP LATCH. REPLACED CABLE AND ADJUSTED CLIPS, OPERATIONAL CHECK OK.May 12, 1997 · N9336 · Doug DC931SDR DHL9780518CFillet Mount · crackedAT C-CHECK, RT WING STA XW-0 FUSELAGE STA 660 FILLET PANEL MOUNT FLANGE CRACKED. REMOVED, FABRICATED FLANGE AND INSTALLED PER SRM 51-1-1.May 11, 1997 · N805DH · Doug DC873FSDR DHL9780506CFillet · delaminatedAT C-CHECK, LT UPPER WING TO FUSE FILLET PANEL 261G IS DELAMINATED. REPAIRED PANEL PER SRM 57-2-0.May 10, 1997 · N805DH · Doug DC873FSDR DHL9780505CFillet · delaminatedAT C-CHECK, RIGHT HAND WING TO FUSELAGE FILLET PANEL 262R DELAMINATED. REMOVED DELAMINATED PANEL, REPAIRED AND REINSTALLED PER SRM 51-3-0.May 10, 1997 · N805DH · Doug DC873FSDR DHL9780504CFillet · delaminatedAT C-CHECK, RIGHT HAND UPPER WING TO FUSE FILLET 262A DELAMINATED. REMOVED AND REPLACED PANEL WITH OVERHAULED PANEL PER SRM 51-3-0.May 10, 1997 · N805DH · Doug DC873FSDR DHL9780503CFillet · delaminatedAT C-CHECK, RT LOWER AFT WING TO FUSE. FILLET PANEL 162X DELAMINATED. REMOVED AND INSTALLED REPAIRED PANEL PER SRM 51-3-0.May 10, 1997 · N805DH · Doug DC873F
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