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 04FDEA01244Thru Bolt · wornTAIL CONE RIGHT HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED TAIL CONE RIGHT HINGE THRU BOLT IAW MM 53-52-00-2 AT MAE.May 12, 2004 · N68051 · Doug DC1010SDR ABXA040183Link · damagedAIRCRAFT VIBRATES AT 320 KTS AT LOW ALTITUDE CLIMB AND CRUISE REGARDLESS OF POWER SETTINGS. REPLACED RT WING TO STRUCTURE TRAILING LINKS AND HARDWARE DUE TO EXCESSIVE MOVEMENT IAW MM 20-10, 20-15 & 20-16.May 11, 2004 · N962AX · Doug DC941SDR EIA2004034Radome · bird strikeJUST AFTER ROTATION AIRCRAFT FLEW THROUGH A FLOCK OF SEAGULLS, IMPACTING SOUNDS HEARD. ALL INSTRUMENT AND ENGINE PARAMETERS NORMAL. NO VISIBLE DAMAGE SEEN FROM CARGO COMPARTMENT. PERFORMED BIRD STRIKE INSPECTION IAW MM 05-51-14. FOUND RADOME DAMAGE BEYOND May 4, 2004 · N471EV · Boeing 747273CSDR DL738040396Fairing · missingWING TO BODY FAIRING PANEL 192JL FOUND MISSING ON ARRIVAL. REPLACED PANEL 192JL.May 4, 2004 · N379DA · Boeing 737832SDR CALA0400458Frame · crackedINSPECTION FOUND A 5 INCH CRACK IN LOWER OUTBOARD AND LOWER I/B CHORDS ON RIGHT W/W AFT SKI JUMP FAIRING. THE CHORDS WERE REMOVED AND REPLACED IAW SRM 51-40-02.May 3, 2004 · N27239 · Boeing 737824SDR CALA0400457Web · crackedINSPECTION FOUND A 5 INCH CRACK IN O/B WEB ON RIGHT W/W AFT SKI JUMP FAIRING. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.May 3, 2004 · N27239 · Boeing 737824SDR CALA0400456Frame · crackedINSPECTION FOUND A 5 INCH CRACK IN LOWER I/B CHORD AND IN LOWER O/B CHORD ON LEFT W/W AFT SKI JUMP FAIRING. NEW CHORDS WERE INSTALLED IAW SRM 51-40-02.May 3, 2004 · N27239 · Boeing 737824SDR CALA0400455Web · crackedINSPECTION FOUND A CRACK IN O/B WEB OF LEFT W/W AFT SKI JUMP FAIRING. THE WEB WAS REPLACED IAW SRM 51-40-02.May 3, 2004 · N27239 · Boeing 737824SDR ANCF200400006Radome · bird strikeBIRD STRIKE AT AIRPLANE'S DOME, THE AIRCRAFT DID NOT SHOW ANY ABNORMAL INDICATION, RADAR WAS TURN OFF AS A PRECAUTIONARY MEASURE. THE RADOME WAS REPLACED IAW AMM 53-51-00 PAG 401 AND ANTENNA TILT POSITION WAS CHECKED AND PERFORMED TEST IAW AMM 34-41-00 PAG 20Apr 9, 2004 · N632CT · Doug MD83SDR UPS04242206Frame · corrodedINSPECTION TYPE: C, FUSELAGE FAIRING 3430 HAS EXTENSIVE CORROSION TO THE FORMED FRAME HOLDING THE ANCHOR NUTS (FWD SIDE OF FAIRING). REPAIR CARRIED OUT IAW SRM 53-10-01, 51-20-01, 51-10-02 & 51-30-02.Apr 6, 2004 · N926UP · Boeing 72731CSDR ASMF200404002Radome · crackedDURING TRANSIT CHECK WAS DETECTED A FOD IMPACT ON RADOME. RADOME HAS AN APPROXIMATELY CRACK OF 24 INCHES PER 20 INCHES. RADOME WAS REPLACED IN ACCORDANCE WITH MM 53-51-00.Apr 1, 2004 · N162PL · Doug MD88SDR ASAA0480194Cam · brokenOKC - FOUND TAILCONE EMERGENCY SLIDE FAILED TO DEPLOY DURING SLIDE DEPLOYMENT TEST PER WORK CARD 28625000. THE FAILURE WAS ATTRIBUTED NOT TO THE SLIDE ASSEMBLY, BUT TO A BROKEN TAILCONE JETTISON AND HOISTING CONTROL CAM. THE CAM WAS REPLACED, BUT THE DEPLOYMMar 25, 2004 · N944AS · Doug DC983SDR ABXA040114Fairing · looseLOW FREQUENCY VIBRATION CAN BE HEARD AND FELT ON FLOOR PANELS. BEGINS AT 320 KTS, BELOW 320 KTS VIBRATION CEASES. TIGHTENED LOOSE FLAP TO BODY FAIRING ON LEFT FLAP ASSY AND ADJUSTED NOSE LANDING GEAR DOOR PRELOAD PER DC9 MM 32-22-01. INSPECTED TABS AND ANTEMar 13, 2004 · N974AX · Doug DC941SDR 04FDEA00587Frame · wornAFT TAIL CONE FWD RT FRAME FOUND 2 EA STOP PLATE WORN. AFT TAIL CONE FWD RT FRAME 2 EA STOP PLATE REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER EA 1-5390-75285. FUSELAGE AERODYNAMIC FAIRING AFT TAILCONE ASSY PLATE.Mar 5, 2004 · N617FE · Doug MD11SDR 04FDEA00544Web · crackedTAIL CONE CENTER FWD WEB FOUND CRACKED. AFT TAILCONE CENTER FWD WEB REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II.Mar 3, 2004 · N617FE · Doug MD11SDR 04FDEA00466Hinge · crackedAFT ACCESSORY COMPARTMENT, LT TAIL CONE LOWER HINGE FITTING SUPPORT FOUND CRACKED. AFT ACCESSORY COMPARTMENT, LT TAILCONE LOWER HINGE FITTING SUPPORT REPAIRED AS PER EA 1-5352-57900, FUSELAGE - TAILCONE/ ACTUATION PLATFORM - PART FABRICATION DEVIATION. CRAFeb 20, 2004 · N586FE · Doug MD11SDR ASAA0480073Release Mech · brokenDURING HV1 CHECK, FOUND TAILCONE RELEASE MECHANISM BROKEN. REPLACED MECHANISM PER MM 53-53-02. (M)Feb 15, 2004 · N976AS · Doug DC983SDR UPS04241872Bracket · damagedINSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLACED IAW SRM 51-20-01.Jan 30, 2004 · N942UP · Boeing 72722CSDR 04FDEA00066Frame · scratchedFWD TAILCONE, LAST FRAME FOUND WITH SCRATCHES. COMPLIED WITH FEDEX EA 1-5300-74174 - FUSELAGE, EXTENDED TAILCONE, FORWARD SECTION, FRAME REPAIR.Jan 7, 2004 · N621FE · Doug MD11SDR MALA040114Radome · dentedDURING INSPECTION IN LCQ, LEFT HAND FWD FUSELAGE AT STA 126 JUST AFT OF RADOME SUSTAINED A DENT. MAINTENANCE REMOVED DENT AT STA 126. PERFORMED HFEC TO DENTED AREA, NO RELEVANT INDICATIONS NOTED. FORMED REPAIR DOUBLER, TREATED AREA, INSTALLED DOUBLER, APPLIDec 30, 2003 · N407XJ · Saab 340BSDR 03FDEA02303Plate · wornTAILCONE AFT SNUBBER TOP AND BOTTOM SUPPORT PLATE FOUND WORN. REMOVED WORN SUPPORT PLATE AS PER SRM 51-31-01 VOL. II AND INSTALLED NEW SUPPORT ASSY AT TAILCONE AFT SNUBBER TOP AND BOTTOM AS PER SRM 51-35-01 VOL. II.Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02301Stiffener · chafedRT TAILCONE UPPER DOOR FORWARD MOST VERTICAL STIFFENER FOUND CHAFED. REMOVED DAMAGED STIFFENER AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW STIFFENER AS PER DRAWING AKC 7868. INSTALLED NEW STIFFENER AT RT TAILCONE UPPER DOOR FED MOST AS PER SRM 51-35-01 Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02300Bracket · chafedRT TAILCONE UPPER DOOR FWD MOST TRIANGULAR VERTICAL BRACKET FOUND CHAFED. REMOVED DAMAGED BRACKET AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW STIFFENER AS PER DRAWING AKC 7868. INSTALLED NEW STIFFENER AT RT TAILCONE UPPER DOOR FWD MOST AS PER SRM 51-31-01Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02297Beam · chafedTAILCONE UPPER DOOR CUTOUT AFT HORIZONTAL BRACKET LT AND RT AREA ADJACENT TO TAIL CONE LADDER SUPPORT FITTING FOUND CHAFED. REMOVED CHAFED SUPPORT AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW BEAM AS PER DRAWING AKC 7528. INSTALLED BEAM AT TAILCONE UPPER DDec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02294Stiffener · chafedLT TAILCONE TOP MOST HORIZONTAL STIFFINER BELOW THE UPPER DOOR HINGE ASSY FOUND CHAFED AT ITS END AREA. LT TAILCONE TOP MOST HORIZONTAL STIFFINER BELOW CHAFED TEE SUPPORT REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II AND DRAWING AKC7543.Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02295Stiffener · chafedRT TAIL CONE TOP MOST HORIZONTAL STIFFENER BELOW THE UPPER DOOR HINGE ASSY FOUND CHAFED AT ITS END AREA. RT TAILCONE TOP MOST STIFFENER BELOW UPPER DOOR HINGE BEAM REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II AND DWG AKC7543.Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02302Beam · chafedTAIL CONE AFT SNUBBER LT AND RT LOWER STIFFENER FOUND CHAFED. REMOVED AND REPLACED TAILCONE AFT SNUBBER LT & RT LOWER STIFFENER AS PER SRM 51-35-01 VOL. II. STIFFENER FABRICATED AS PER DWG AKC7591.Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02298Stiffener · chafedTAILCONE RT FWD MOST EDGE TOP STIFFENER FOUND CHAFED. TAILCONE RT FWD MOST EDGE TOP CHAFED DOUBLER REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II.Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02296Panel · chafedRT TAILCONE UPPER DOOR FORWARD MOST ACCESS PANEL FOUND CHAFED. RT TAILCONE UPPER DOOR FWD MOST ACCESS PANEL FABBRICATED AS PER DWG AKC 7506. PANEL REMOVED AND REPLACED AS PER MM 20-50-02.Dec 26, 2003 · N584FE · Doug MD11SDR 03FDEA02189Frame · debondedAFT TAIL CONE INTERIOR LEFT SIDE FRAME ASSEMBLY FOUND DISBONDED. AFT TAIL CONE INTERIOR LT SIDE FRAME ASSEMBLY CARRIED OUT. REPAIR AS PER FEDEX EA 1-5240-75188, SERVICE DOORS, AFT EXTENDED TAILCONE PANEL ASSY REPAIR.Dec 14, 2003 · N608FE · Doug MD11SDR AWXA200301584Skin · debondedMCN - MINOR REPAIR - DURING C-18 CHECK A FOUND UPPER SURFACE OF TAIL CONE DISBONDED 28 INCHES FROM FORWARD EDGE BS 1185 TO BS 1188, WL 289. MAINTENANCE PREPARED TAIL CONE UPPER SURFACE BS 1185 TO BS 1188, WL 289; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-1Dec 7, 2003 · N325AW · Boeing 737301SDR DHL2003802573Skin Panel · delaminatedLEFT WING TO FUSELAGE NR 706 PANEL EXTERNAL SKIN DELAMINATED STA 912.000 - STA 980.000. REMOVED DELAMINATED PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED LPS3 IAW SRM 51-1-8 PG 35-36. INSTALLED NEW PANEL ASSY ON LEFT Dec 4, 2003 · N802DH · Doug DC873SDR 03FDEA02003Frame · crackedFORWARD TAIL CONE MOST AFT STA 2244 (UPPER HINGE AREA) FRAME FOUND CRACKED. FRAME AND ANGLE REPAIRED AS PER SRM 53-00-01 FIG. 9 VOL. I AND SRM 51-31-01 VOL. II.Nov 30, 2003 · N608FE · Doug MD11SDR 03FDEA02002Frame · crackedFORWARD TAIL CONE MOST AFT STA 2244 LOWER RT SIDE FRAME FOUND CRACKED. TRIMMED OUT DAMAGED FRAME AS PER SRM 53-00-01, FIG.9, VOL.I. FABRICATED FRAME AS PER DRAWING AKC5739. FABRICATED REPAIR ANGLE AS PER SRM 53-00-01, FIG.9, VOL.I. INSTALLED FRAME AND RNov 29, 2003 · N608FE · Doug MD11SDR LR7A03090Fairing · crackedDURING SCHEDULED C4 INSPECTION, FOUND FS 476 AERODYNAMIC FAIRINGS CRACKED AT LBL 30 AND RBL 30, WL 283. REPAIRED IAW SRM SMP 583 51-140-12. NR 2060.Nov 21, 2003 · N404LC · Lkheed 382GSDR GLBA2003145Radome · bird strikeBIRD STRIKE, DAMAGED RT I/B WING, RT O/B WING AND RADOME. REPLACED LT INBD LEADING EDGE PN 114-120028-23Nov 5, 2003 · N195GL · Beech 1900DSDR CA031104003Casting · misinstalled(CAN) ON DISASSEMBLY OF THE AIRCRAFT FOR REPAIR, THE PART WAS FOUND NOT TO BE ATTACHED TO IT'S MATING FAIRING AS REQUIRED. THE RIVETS WERE PULLED BETWEEN THE ATTACHING PARTS AND NOT THROUGH THE CASTING.Nov 4, 2003 · Bell 407SDR AWXA200301342Tail Cone · delaminatedMCN - MINOR REPAIR - DURING C-21 CHECK THE TAIL CONE WAS FOUND DELAMINATED AT LOWER CENTER 7 INCHES, 11 INCHES, & 24 INCHES FROM FORWARD END, 7.5 INCHES LT LOWER SIDE 12.5-15 INCHES FROM FORWARD END, 4-7 INCHES RT SIDE OF CENTER LOWER 16.5 INCHES FROM FORWARD Oct 22, 2003 · N182AW · Boeing 737277SDR GTIA030867Hinge · brokenFOUND TAILCONE RELEASE ARM DOOR IN AFT F/A STATION BROKEN. RESECURED HINGE. REPLACED RIVETS. (M)Oct 21, 2003 · N811NK · Doug DC981SDR DLM88030922Tail Cone · unsecureOPS REPORTED TAIL CONE HANGING FROM A/C. CONTRACT MTC FOUND TAIL CONE PARTIALLY DEPLOYED. ONE PIN STILL ENGAGED. SLIDE DID NOT DEPLOY AND WAS DISCONNECTED. TAIL CONE REMOVED AND REINSTALLED.Oct 12, 2003 · N999DN · Doug MD88SDR CALA0300590Support Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING TO BODY FAIRING SUPPORT ANGLE AT BS 535. THE ANGLE WAS REPAIRED IAW ECRA 5350-01227.Oct 12, 2003 · N12313 · Boeing 7373T0SDR SIMA200328801Radome · bird strikeDURING TAKEOFF FROM BUF, CREW REPORTED A BIRD STRIKE TO THE NOSE AREA. MAINTENANCE REMOVED AND REPLACED FRAMES 3, 4, 5 AND 6, STRINGER 4R, RIGHT FORWARD NOSE TOP SKIN PANEL, RIGHT AFT NOSE TOP SKIN PANEL IAW EMB SRM 51-42-01 AND REPAIRED SKIN FORWARD OF RIGHTOct 10, 2003 · N618AE · Emb EMB145LRSDR AWXA200301258Skin · debondedDURING C-17 CHECK 8 AREAS OF TAIL CONE SURFACE WERE FOUND DEBONDED. MAINTENANCE CUTOUT DAMAGE ON TAIL CONE SURFACE AT BS 1176 CENTERLINE, BS 1166.5, 6 INCHES RT OF CENTER, BS 1169 2.5 INCHES RT OF CENTER, BS 1163.5, 3 INCHES RT OF CENTER, BS 1165.5 11INCHES LTOct 6, 2003 · N156AW · Boeing 7373G7SDR AWXA200301256Skin · debondedMCN - MINOR REPAIR - DURING C-17 CHECK FOUND TOP CENTER AREA OF TAIL CONE DISBONDED, 18 INCHES-22 INCHES FROM FORWARD EDGE. MAINTENANCE CUTOUT DISBONDED AREA OF TOP CENTER TAIL CONE, 18 INCH-22 INCHES FROM FORWARD EDGE AND PERFORMED A BOND REPAIR IAW B737-300 Sep 29, 2003 · N326AW · Boeing 737301SDR AWXA200301167Angle · crackedDURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON WING TO BODY FAIRING VERTICAL ATTACH ANGLE, AFT OF FR 34 LT, BELOW LOWER FASTENER HOLE. MAINTENANCE REMOVED AND REPLACED VERTICAL ATTACH ANGLE AT FR 34 LT IAW A320 SRM 51-42-11 PG 21-22, FIG 8.Sep 25, 2003 · N650AW · Airbus A320232SDR AWXA200301170Plate · crackedMCN - MINOR REPAIR - DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON LT WING TO BODY FAIRING SUPPORT STRUCTURE CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CLOSING PLATE AT FR 34, AND U-CHANNEL ABOVE CLOSING PLATE; FABRICATED A NEW REPLACEMENT CLOSING PLATE ASep 24, 2003 · N650AW · Airbus A320232SDR AWXA200301165Plate · crackedDURING C-04 CHECK A .25 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING SUPPORT STRUCTURE CLOSING PLATE AT FR 34. MAINTENANCE REMOVED CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7, SECT 6,Sep 24, 2003 · N650AW · Airbus A320232SDR A6WA200340137Tail Cone · damagedDAMAGE TO TAIL CONE, RESULTING IN DELAMINATION OF INNER AND OUTER SKINS AND CORE DAMAGE. REPAIR, FABRICATED SKIN PLIES TWO EACH AND EXTRA PLY ONE EACH FOR EACH DAMAGED SKIN FROM KEVLAR 49 STYLE 281 FABRICATED PREPEG CMS532-01. EXTRA PLY TO EXTEND .5 INCHES PSep 18, 2003 · N441ZW · Cndair CL6002B19SDR CALA0300532Cable · out of adjustTHE TAIL CONE INNER RELEASE HANDLE REQUIRED EXCESSIVE FORCE TO PULL. THE TAIL CONE CABLE WAS ADJUSTED, CLEANED AND LUBRICATED IAW MM 53-53-00. AN OPERATIONAL CHECK WAS GOOD.Sep 17, 2003 · N16806 · Doug DC982SDR CALA0300531Handle · lack of lubeTHE TAIL CONE HANDLE AFT ENTRY DOOR REQUIRED EXCESSIVE FORCE TO OPEN. THE DOOR HINGES AND HANDLE MECHANISM WERE LUBRICATED. A PULL TEST WAS PERFORMED IAW MM 53-53-00 AND OPERATIONAL CHECKS WERE GOOD.Sep 17, 2003 · N16806 · Doug DC982
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