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 03FDEA00392Pin · looseTAILCONE LT SIDE MATING FLANGE UPPER ALIGNMENT PIN HOLE FOR THE PIN HAS EXCESSIVE PLAY. REMOVED FILLER AND PIN IAW SRM 51-31-01. FAB NEW FILLER IAW SRM 53-30-00 FIG 1, INSTALLED IAW SRM 51-31-01.Apr 5, 2003 · N317FE · Doug DC1030SDR 03FDEA00394Seal · crackedNR 655 TAILCONE FWD UPPER LT METAL SEAL CRACKED ANS CHAFED. CLOSING ACTION ON 04/05/03. REMOVED LT FWD UPPER METAL SEALS 2EA. FROM TAILCONE IAW SRM 51-31-01, RECEIVED REPLACMENT SEALS ON ATTACHED TRAVELER NR T2/324508. INSTALLED REPLACEMENT SEALS IAW SRMApr 5, 2003 · N317FE · Doug DC1030SDR UPS03M40720Skin · corrodedINSPECTION TYPE: C, AFT ACCESSORY COMPT ZONE 316 RT FAIRING ATTACHMENT ANCHOR NUT SKIN FOUND CORRODED. RT FAIRING ATTACHMENT ANCHOR NUT SKIN REMOVED AND FOUND OUT OF LIMIT PER SRM 53-00-01 VOL I REV 32. CORROSION BLEND OUT AREA TRIMMED PER EN:10 06-03. HFEApr 3, 2003 · N271UP · Doug MD11SDR GTIA030160Control Cable · out of rigTAILCONE WILL NOT RELEASE WHILE ACCOMPLISHING STEP D OF WORKCARD N53038. RE-RIGGED TAILCONE PULL CABLE AT THE PULL CABLE HOUSING, OPS CHECKED GOOD.Mar 13, 2003 · N816NK · Doug DC982SDR QXEA0300346Panel · chafedPDX - CHAFING ON PANEL ATTACH FLANGES, PANEL 262FT, ENTIRE FORWARD EDGE OF PANEL FLANGE. REPAIRED IAW HORIZON AIR EA 6-57-122 AND RD 8/4-57-143.Mar 9, 2003 · N404QX · Bombdr DHC8401SDR QXEA0300343Panel · chafedPDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261LT, AFT FLANGE BETWEEN CAMLOCK HOLES 1-5. REPAIRED IAW HORIZON AIR EA 6-57-122 AND RD 8/4-57-144.Mar 8, 2003 · N404QX · Bombdr DHC8401SDR QXEA0300342Panel · chafedPDX - CHAFING ON PANEL ATTACH FLANGE OF PANEL 261FT, AFT FLANGE, BETWEEN CAMLOCK HOLES 1-6. REPAIRED IAW RD 8/4-57-144.Mar 8, 2003 · N404QX · Bombdr DHC8401SDR QXEA0300341Panel · chafedPDX - CHAFING ON PANEL ATTACH FLANGE OF PANEL 261CT, AFT EDGE AT FIRST FIVE CAMLOC HOLES. REPAIRED IAW HORIZON AIR EA 6-57-122.Mar 8, 2003 · N404QX · Bombdr DHC8401SDR QXEA0300339Panel · chafedPDX - PANEL 261FT IS LIGHTLY CHAFED THROUGH PAINT ON TRAILING EDGE. REPAIRED IAW RD 8/4-53-457 AND DHC-8 SRM 51-21-10.Mar 8, 2003 · N404QX · Bombdr DHC8401SDR CALA0300107Cable · out of rigTHE TAILCONE FAILED TO DROP WITHIN SPECIFICATIONS AT ALL THREE POSITIONS DURING FUNCTIONAL TEST. THE PULL EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW 53-53-00.Mar 8, 2003 · N17812 · Doug DC982SDR QXEA0300332Flange · chafedPDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261FT, AFT FLANGE, BETWEEN CAMLOC HOLES. BLENDED DAMAGED AREA.Feb 27, 2003 · N404QX · Bombdr DHC8401SDR QXEA0300326Panel · chafedPDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261CT, AFT EDGE, AT FIRST FIVE CAMLOC HOLES FROM OUTBOARD EDGE. BLENDED DAMAGED AREA.Feb 27, 2003 · N404QX · Bombdr DHC8401SDR QXEA0300325Panel · chafedPDX - CHAFING ON PANEL ATTACH FLANGE, PANEL 261LT, AFT FLANGE BETWEEN CAMLOC HOLES 1-5. BLENDED DAMAGED AREA.Feb 27, 2003 · N404QX · Bombdr DHC8401SDR ASAA0380141Fillet · corrodedOAK - DUIRNG C-CHECK, FOUND CORROSION ON LEFT WING-TO-BODY FAIRING FILLET PANEL 2108. INSTALLED DOUBLER AT FS 1079-1098 PER SRM 53-04. (M)Feb 22, 2003 · N964AS · Doug DC983SDR CALA0300061Cable · frayedTHE TAILCONE FAILED TO SEPARATE FROM AIRCRAFT WHEN USING AFT ENTRANCE DOOR TO DEPLOY TAILCONE. FOUND L/H TAILCONE RELEASE CABLE FRAYED IN TWO PLACES WHERE IT PASSES OVER UPPER PULLEY. REPLACED CABLE AND PERFORMED ADJUSTMENT TEST OF TAILCONE SYSTEM IAW MM 53-53Feb 21, 2003 · N72822 · Doug DC982SDR DLM88030168Radome · crushedBIRD STRIKE ON APPROACH RWY19R APPROX 400 FT AGL 126 KTS REPLACED RADOME WITH PART BORROWED FROM A/AFeb 20, 2003 · N919DL · Doug MD88SDR DHL2003804775Fillet · delaminatedLT WING, WING TO FUSELAGE FILLET INNER SKIN DELAMINATED , STA 826.000 - STA. 912.000. R & R PANEL ON LT WING, WING TO FUSELAGE STA. 826.000-STA. 912.000 IAW SRM 51-3-0 PG. 1Feb 12, 2003 · N804DH · Doug DC873FSDR DHL2003804879Fairing · delaminatedRT WING NR 709 AFTER WING FUSELAGE FILLET EXTERNAL SKIN DELAMINATED STA 108.000 - STA 120.000. REMOVED DELAMINATED PANEL (RT WING STA 108.000 - 1120.000) IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, INSTALLED NEW PANEL (FROM USA) IAFeb 7, 2003 · N804DH · Doug DC873FSDR OIZ2003F00002Angle · crackedDURING THE ACCOMPLISHMENT OF THE A.D., A SMALL CRACK WAS FOUND IN THE LEFT VERTICAL TO HORIZONTAL STABILIZER FAIRING ANGLE. THE CRACK WAS LOCATED IN THE APPROXIMATE CENTER OF THE ANGLE AND ALONG THE UPPER SECTION (HORIZONTAL STABILIZER SIDE) OF THE BEND RADIUFeb 4, 2003 · N381CR · Beech 1900CSDR OIZ2003F00001Angle · crackedDURING THE ACCOMPLISHMENT OF AD, A SMALL CRACK WAS FOUND IN THE LEFT VERTICAL TO HORIZONTAL STABILIZER FAIRING ANGLE. THE CRACK WAS LOCATED IN THE APPROXIMATE CENTER OF THE ANGLE AND ALONG THE UPPER SECTION (HORIZONTAL STABILIZER SIDE) OF THE BEND RADIUS. THFeb 4, 2003 · N381CR · Beech 1900CSDR AWXA200300074Seal · tornENROUTE A FLIGHT ATTENDANT NOTICED CONSIDERABLE VIBRATION DURING ENTIRE FLT BETWEEN ROWS 11-17. REPORTS INDICATE VIBRATIONS COULD BE FELT ABOVE AND BELOW 290 KTS. MAINTENANCE FOUND LT UPPER MID WING TO BODY FAIRING SEAL HAD OLD STYLE OF OF SEAL INSTALLED AND TJan 25, 2003 · N621AW · Airbus A320231SDR COMA0360039FairingFLIGHT 5877 RUMBLING NOISE AND VIBRATION FELT IN AIR FRAME.REPLACED MISSING SEALANT AT WING TO FUSELAGE FAIRING.Jan 20, 2003 · N435CA · Cndair CL6002B19SDR UPS03240094Frame · corrodedINSPECTION TYPE: C&SI, FAIRING 3429 HAS CORRODED FRAME SECTION ABOVE ACCESS PANEL 3420. CUTOUT CORRODED FRAME SECTION, REMOVED IAW SRM 51-30-2. NEW FRAME SECTION FABRICATED IAW SRM 51-20-1 FIG 7 AND SRM 53-50-1 FIG 2. NEW FRAME SECTION INSTALLED IAW SRM 51-Jan 17, 2003 · N945UP · Boeing 72722CSDR CALA0300012Clip · out of adjustTHE FORCE REQUIRED TO PULL EXTERIOR TAIL CONE RELEASE HANDLE FROM ITS RETAINING CLIPS EXCEEDED 35 POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND PULL WAS WITHIN LIMITS AT 25 POUNDS.Jan 16, 2003 · N69826 · Doug DC982SDR QXEA0300059Panel · chafedPDX-FORWARD FLANGE OF PANEL 262FT IS CHAFED. REPAIRED IAW DHC-84 SRM 51-21-10, SRM 51-25-10 AND HORIZON AIR EA 6-53-173.Jan 11, 2003 · N400QX · Bombdr DHC8401SDR AWXA200300083Plate · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CLOSING PLATE FRAME 34. MAINTENANCE REMOVED CRACKED RT WING TO BODY FAIRING SUPPORT STRUCTURE ANGLE CLOSING PLATE AT FR 34; FABRICATED A NEW REPLACEMENT CLOSING PLATEJan 7, 2003 · N647AW · Airbus A320232SDR HEEA083502Duct · crackedAIR INLET DUCT CRACKED. TO BE SENT TO VENDOR.Jan 7, 2003 · N854PH · Aerosp AS355*SDR CALA0200583Cable · frayedTHE TAILCONE RELEASE AT EXTERIOR AND INTERIOR HANDLES PULLED HIGH. THE UPPER L/H TAILCONE JETTISON CABLE WAS FOUND WORN AND FRAYED AT UPPER FORWARD PULLEY. REMOVED AND REPLACED CABLE ASSEMBLY. RIGGED AND ADJUSTED TAILCONE RELEASE SYSTEM IAW MM 53-53-00.Dec 11, 2002 · N72830 · Doug DC982SDR CALA0200564Cable · frayedTHE TAILCONE DROP TEST FAILED AT EACH OF THREE LOCATIONS. MAINTENANCE FOUND THE LEFT UPPER TAILCONE JETTISON CABLE FRAYED IN TWO PLACES. THE CABLE WAS REMOVED AND REPLACED. PERFORMED ADJUSTMENT OF TAILCONE RELEASE SYSTEM IAW MM 53-53-00.Nov 25, 2002 · N98876 · Doug DC982SDR SWIA200211469Fairing · damagedFLAPS FAIL AT ''0'' DURING APPROACH TO LANDING. REMOVED AND REPLACED LT INBOARD FLAP TO FUSELAGE FAIRING IAW SRM 51-71-00.Nov 11, 2002 · N916SW · Cndair CL6002B19SDR F3LA200200365Tail Cone · dentedDURING C 2 CHECK, A DENT WAS FOUND ON THE LT SIDE OF THE TAIL CONE, NEAR THE ELEVATOR ATTACH POINTS. DENT WAS REPAIRED AND PAINTED IAW MAINTENANCE MANUAL 737-300 MM 51-21-99 AND SRM 51-70-06.Oct 18, 2002 · N313FL · Boeing 737300SDR C2XA02SH102Fairing · crackedSHV- DURING C CHECK, RT FAIRING ON APU FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED RT FAIRING IAW CONTINENTAL EXPRESS EC 5350-01032. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.Oct 17, 2002 · N14939 · Emb EMB145ERSDR ASAA0280319Rub Strip · crackedOAK - FOUND DURING C-CHECK, LEFT WING TO BODY FAIRING AFT FILLET 2108 CHAFE STRIP WAS CRACKED AT TOP SIDE. TRIMMED CRACK AREA AND BLENDED AREA FILLET PANEL PER SRM 53-01. (M)Sep 20, 2002 · N953AS · Doug DC982SDR CALA0200454Control Cable · out of adjustTHE EXTERIOR TAIL CONE RELEASE HANDLE PULLED LOW AT 10 POUNDS. THE TAIL CONE CABLE TENSION WAS ADJUSTED AND THE HANDLE CLIPS WERE REPLACED.Sep 7, 2002 · N71828 · Doug DC982SDR UPS02239115Stiffener · crackedINSPECTION TYPE:C WING TO BODY FAIRING 3409 HAS A CRACKED FWD FRAME STIFFENER ANGLE. FABRICATED AND INSTALLED NEW STIFFENER IAW SRM 53-50-1 FIG 4 AND SRM 51-2 0-1 FIG 7.Aug 13, 2002 · N926UP · Boeing 72731CSDR P5CA0200696Panel · damagedFOUND 6 INCH CRACK IN HONEYCOMB OF PANEL 193 AFT OF LT BODY GEAR FAIRING PANEL. REPAIRED PANEL AFT OF LT BODY GEAR BS 1620 TO BS 1660 AS PER B747 SRM 51-40-07. LT BODY GEAR O/B STRUT DOOR DAMAGED. DOOR REMOVED, INSTALLED NEW DOOR ASSY. REINSTALLED LEFT BODAug 10, 2002 · N355MC · Boeing 747341SDR UPS02439112Web · corrodedINSPECTION TYPE:C FX- AIR CONDITIONING BAY REAR FIXED FAIRING INTERIOR REAR SURFACE FOUND SURFACE CORROSION AT STA 1255 RBL 9 TO RBL 30. REAR FIXED FAIRING REAR WEB AND SUPPORT CHORD REPAIRED AS PER SRM 51-40-02 FIG 1, 51-40-03 FIG 2 AND FIXED PNL REPLACED PEAug 2, 2002 · N526UP · Boeing 747212BSDR UPS02239016Frame · corrodedINSPECTION TYPE:C CORROSION ON FAIRING # 3334 ON FRAME AT L/H FAN INLET DOOR AFT AREA FRAME REPAIR CARRIED OUT IAW SRM 51-40-4 L/H FAN INLET DOOR REPLACED IAW MM 21-52-51 & DOOR ACTUATING ROD REP LACED IAW MM 21-52-51Jul 30, 2002 · N928UP · Boeing 72722CSDR AWXA200200700Rib · crackedLCQ - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND AT L/H AFT WING TO BODY FAIRING SUPPORT RIB BS 1300. MAINTENANCE REMOVED CRACKED AREA OF SUPPORT RIB, FABRICATED 2 EACH REPAIR ANGLES, AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-71, PG. 201-204.Jul 29, 2002 · N904AW · Boeing 7572S7SDR DHL2002806857Panel · delaminatedLOWER FUS FILLET NR 742 LT EXTERNAL SKIN DELAMINATED. REMOVED FILLET NR 742 LT IAW SRM 51-3-0 PG 1. INSTALLED NEW FILLET PANEL IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 1.Jul 23, 2002 · N806DH · Doug DC873FSDR CALA0200389Latch · out of rigTHE TAILCONE INTERIOR RELEASE HANDLE PULL WAS EXCESSIVE. THE TAILCONE LATCH LOCKPINS WERE ADJUSTED AND OPERATION CHECKED GOOD IAW MM 53-53-00.Jul 2, 2002 · N14839 · Doug DC982SDR UPS02838910Fitting · crackedINSPECTION TYPE:C2 TAIL CONE ATTACH FITTING HAS CRACK AT L10L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21.Jun 26, 2002 · N802UP · Doug DC873FSDR DLM88020667Tail Cone · departedAT PUSHBACK GOT TAIL CONE UNSAFE MESSAGE WITH ASSOCIATED TAILCONE SEPARATED FROM A/C AND LYING ON GROUND BEHIND THE ACA. INSTALLED NEW TAILCONE PER M/M AND REMOVED AND INSTALLED NEW SLIDE PACK.Jun 14, 2002 · N976DL · Doug MD88SDR CALA0200333Cable · out of rigTHE TAIL CONE DID NOT DROP WHEN USING AFT CABIN DOOR TAIL CONE EMERGENCY RELEASE. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-00.Jun 8, 2002 · N83872 · Doug DC982SDR UPS02M38951Frame · crackedINSPECTION TYPE:C, EXTENDED TAIL CONE AFT CONE GUIDE PIN LOCATING BLOCK ATTACHMENT FRAME AT CANT STA 2258.846 FOUND CRACKED. EXTENDED TAIL CONE CRACKED AREA TRIMMED AND REPAIR CHANNELS AND ANGLES FABRICATED AS PER SRM 53-00-01 FIG 9 VOL I REV 31. REPAIR CHANMay 29, 2002 · N253UP · Doug MD11FSDR SIMA200214103Fairing · corrodedSAW - DURING CPCP4 INSPECTION, MAIN LANDING GEAR FAIRING AT FRAME 27A HAS CORROSION. REPAIRED CORRODED AREA IAW ATR 42 SRM 53-91-43 PAGES 430 THROUGH 433. AIRCRAFT RETURNED TO SERVICE. (M)May 17, 2002 · N282AT · Aerosp ATR42300SDR MWEA020323Radome · damagedFOUND RADOME DAMAGE ON POST FLIGHT WALKAROUND. REMOVED AND REPLACED RADOME.May 7, 2002 · N807ME · Doug DC981SDR MEX2002253Radome · separatedFLT 477 - IAH-MEX - DURING LANDING CAPTAIN FELT A HIT TO THE AIRCRAFT. AT TRANSIT CHECK THE NOSE COWLING OF THE RIGHT ENGINE WAS FOUND WITH A DAMAGE IN ITS UPPER PART OF APPROXIMATELY 15 INCHES OF LENGTH OF 4 INCHES OF CUTTING, ALSO 5 BLADES WERE OUT OF LIMITApr 8, 2002 · N1003X · Doug DC982SDR COOSDR02076Tail Cone · delaminatedFUSELAGE TAIL CONE WITH DELAMINATION AT THE OUTER SURFACE.Apr 1, 2002 · N813US · Doug DC981SDR GTIA020400Attach Fitting · corrodedFTW - FOUND TAIL CONE BENT UP AT HOUSING TAIL CONE ATTACH PLATE SHEAR, 12 PLACES. UPON INSPECTION, FOUND ATTACH PLATE CORROSION. FORMED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS. (M)Mar 30, 2002 · N806NK · Doug DC981
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