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 MALA020206Skin · dentedDENT IN LT TAIL CONE AREA STA 803, .042 DEEP. MAINTENANCE REPAIRED DENT IAW EO S53117.Mar 22, 2002 · N447XJ · Saab 340BSDR P5CA00200666Skin · crackedCRACK FOUND IN BODY TAIL LOWER SKIN AT STATION 2280. CRACK CUT OUT, PACKER FITTED & NEW REPAIR DONE ON OUTER SKIN AS PER SRM 53-30-03.Mar 18, 2002 · N854FT · Boeing 747122SDR LR7A02019Longeron · brokenDURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND LMLG WHEEL WELL LBL 85 LONGERON BROKEN AT FS 477, WL 200.REPAIRED IAW SRM SMP 583 53-40-42. NR 2094.Mar 7, 2002 · N403LC · Lkheed 382GSDR COOSDR010154Skin · delaminatedRIGHT WING TO BODY FAIRING OUTER SKIN DELAMINATED.Mar 1, 2002 · N79751 · Boeing 7272M7SDR COOSDR010149Skin · delaminatedRIGHT WING TO BODY FAIRING SKIN DELAMINATED.Mar 1, 2002 · N79751 · Boeing 7272M7SDR 2002F00239Gasket · missingFLT TPU020 - UOI/GYE - DURING CLIMB, CABIN PERSONNEL DETECTED A NOISE AT THE PAX CABIN, NEAR THE EMERGNCY OVERWING EXIT DOORS. THE AIRCRAFT CONTINUE ITS FLIGHT TO GYE STATION. AFTER LANDING AT GYE STATION, TECHNICIANS PERFORMED INSPECTION OF THE AIRCRAFT, ANFeb 24, 2002 · N463TA · Airbus A320233SDR SWIA200210577Tail Cone · out of positionCONTROL YOKE BINDS ABOUT HALFWAY THROUGH FORWARD AND AFT TRAVEL WITH ELEVATOR TRIM IN THE GREEN ARC. BIND IS LESS WITH ELEVATOR TRIM FULL FORWARD AND GOES AWAY COMPLETELY WITH TRIM FULL AFT. REPOSITIONED TAIL CONE TO PREVENT RUBBING ON ELEVATOR. OPS CHECK GJan 19, 2002 · N190SW · Emb EMB120ERSDR QXEA0200062Frame · crackedPDX - REAR TAIL SECTION INTERNAL FRAME 4 STRINGER 4 HAS CRACK NEAR STATION 700.409. REPAIRED IAW DHC-8 RD 8-55-199.Jan 7, 2002 · N355PH · Dhav DHC8202SDR QXEA0200061Frame · crackedPDX - REAR FUSELAGE TAIL CONE INTERNAL TOP STRUCTURE FRAME FOUR CASTELLATION IS CRACKED AT STRINGER 4R. REPAIRED IAW DHC-8 RD 8-55-199.Jan 7, 2002 · N355PH · Dhav DHC8202SDR COMA0260036Fitting · crackedRIGHT HAND HORIZONTAL STABILIZER VISOR FITTING CRACKED.REPAIRED I/A/W 601R-55-11-016.Jan 1, 2002 · N973CA · Cndair CL6002B19SDR 2001UALA02478Skin · crackedTHE TAIL CONE LOWER SKIN HAS CRACK AND DENT JUST AFT OF THE APU COMPARTMENT. MAJOR REPAIR ACCOMPLISHED INSTALLED REPAIR DOUBLER.Dec 30, 2001 · N198UA · Boeing 747422SDR 01FDEA01048Bracket · crackedN 1391 BRACKET CRACKED UNDER #4 CARGO TRACK AT BS 950A, BL0, WL 207. R&R BRACKET PER SRM 51-30-2.Dec 10, 2001 · N241FE · Boeing 727277SDR 01FDEA01062Bracket · crackedN 311 SUPPORT BRACKET CRACKED FOR FUSELAGE FAIRING BS 720E, STR 28L. ** S/D ** COMINGDec 9, 2001 · N241FE · Boeing 727277SDR QXEA0101997Support · bentPDX - BENT FAIRING SUPPORT STRUCTURE IS BENT. REPAIRED IAW FOKKER SRM 53-53-11, PAGE 35, ITEM 265, SRM 51-10-4, PARAGRAPH 4 B AND C.Nov 16, 2001 · N482US · Fokker F28MK4000SDR UPS01837253Doubler · corrodedINSPECTION TYPE:C2 TAIL CONE INNER DOUBLER AT 62 ACCESS HOLE, AND LT OUTER SKIN IS CORRODED BEYOND LIMITS STA 1861-1890 APPROX. REMOVED, FABRICATED, AND REPLACED DOUBLER AND SKIN SECTION IAW DWG 5704650, AND SRM 53-1-0, 51-1-21, 51-1-20D.Oct 17, 2001 · N718UP · Doug DC871FSDR MWEA011373Pin · wornTAIL CONE REQUIRED EXCESSIVE FORCE DURING OPERATIONAL CHECK. REROUTED CABLE AND REPLACED WORN GUIDE PINS.Oct 10, 2001 · N600ME · Doug DC914SDR LR7A01083Strut · elongatedDURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG WL 200 LONGERON 2 EA. ELONGATED HOLES AT FS 523, RBL 75.REPAIRED IAW LAC MEA 382-53-01-061. NR 0211.Oct 9, 2001 · N402LC · Lkheed 382GSDR DHL2001742509Skin · damagedAT C-CHECK, TAIL CONE UPPER SIDE RT AFT AREA. SKIN HAS THREE SMALL HOLES. (RED MARKED)Oct 4, 2001 · N742DH · Boeing 727225SDR CALA0100894Clip · out of adjTHE TAILCONE EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.Sep 23, 2001 · N35836 · Doug DC982SDR MWEA011252Warning System · malfunctionedTHE TAIL CONE WARNING LIGHT ILLUMINATED. EXECUTED A LOW SPEED ABORT. NR 3 AND 4 BRAKES WERE SMOKING AFTER RTO. BRAKE TEMPS NEVER EXCEED 400 DEGREES AND OVERHEAT LIGHT NEVER CAME ON. DEFERRED TAIL CONE ANNUNCIATOR SYSTEM PER MEL 53-1B T-FUNCTION C/W. REINSSep 10, 2001 · N806ME · Doug DC981SDR COMA0160652Radome · burnedFLIGHT #5628. DURING CRUSIE FLIGHT AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE, CREW REPORTED SMOKE/BURNING SMELL IN CABIN AND GALLEY AREA. AIRCRAFT CONTINUED FLIGHT TO IAD AND LANDED SAFELY.REPLACED THE RADOME.Aug 26, 2001 · N943CA · Cndair CL6002B19SDR DHL2001804511Fairing · delaminatedD-CHECK, FUSELAGE FILLET NR 261H EXTERNAL SKIN DELAMINATED 2 INCHES. REPAIRED LT WING TO FUSELAGE FILLET NR 261H EXTERNAL SKIN WITH HYSOL & ARALDITE IAW SRM 51-1-9 PG 1-2.Aug 10, 2001 · N804DH · Doug DC873FSDR DHL2001804508Fairing · crackedD CHECK - RT UPPER SECTION, FAIRING CRACKED 3 INCHES AT STA 1849.250. CUT FAIRING DAMAGED AREA FABRICATED FILLER & DOUBLER, AND INSTALLED IAW SRM 53-2-0 FIG 1B.Aug 10, 2001 · N804DH · Doug DC873FSDR UPS01236680Frame · corrodedINSPECTION TYPE:C BODY FAIRING #3430 HAS CORRODED FRAME AT R/H GND FAN LOUVRE DOOR AFT CUTOUT. FRAME FABRICATED AND INSTALLED PER SRMAug 9, 2001 · N908UP · Boeing 72727CSDR 2001UALA01446Nut Plate · looseVIBRATION AT M .80, INCREASES WITH AIRSPEED, AND LEFT TURNS, STAYS THE SAME WITH SPOILERS EXTENDED. FOUND NUTPLATES ON TAIL CONE REQUIRING REPLACEMENT. NUTPLATES ALLOWED TAIL CONE TO VIBRATE.Jul 19, 2001 · N7275U · Boeing 727222SDR DHL2001803507Structure · crackedTAIL CONE-RT ELEVATOR BRUSH COVER INNER STRUCTURE CRACKED 1.25. PERFORMED STOP HOLE PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER WITH ALCLAD (2420T3 0.025) PER SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED PER SRM 51-1-8, INSTALLED DOUBLER PER SRM 53-20 FIG 1Jun 30, 2001 · N803DH · Doug DC873SDR ZW0A0104101Tail Cone · departedDURING TAKEOFF ON A TEST FLIGHT OUT OF A MAJOR CHECK, THE TAIL CONE UNSAFE LIGHT ILLUMINATED. CREW ELECTED TO GO AROUND AND LAND. DURING LANDING THE TAIL CONE DEPARTED FROM THE AIRCRAFT AND LANDED ON THE RUNWAY, AND THE TAIL CONE EVACUATION SLIDE DEPLOYED. Jun 24, 2001 · N9615W · Doug DC983SDR DHL2001803536Fairing · crackedAT C-CK, RT WING TO FUSELAGE UPPER FAIRING SHOWS 1 INCH BREAK AT STA 834.Jun 18, 2001 · N803DH · Doug DC873SDR DHL2001803537Radome · crackedAT C-CK, RADOME- 2 (EA) .25 INCH CRACKS ON RADOME LOWER LIP (INNER PART). PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.Jun 14, 2001 · N803DH · Doug DC873SDR ABXA010563Skin · corrodedTAILCONE HAD CORROSION AND DETERIORATING SEALANT JUST ABOVE THE LOWER TAILCONE LIGHT IN THE SEAM. REPAIRED AREA AND INSTALLED NEW SKIN IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-11, AND DC-8 DWG 5704665.Jun 5, 2001 · N818AX · Doug DC863SDR CALA0100498Clip · out of adjTHE CABIN AFT ENTRY DOOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.May 23, 2001 · N16895 · Doug DC982SDR CALA0100497Clip · out of adjTHE EXTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS LOW. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.May 23, 2001 · N16895 · Doug DC982SDR CALA0100496Clip · out of adjTHE INTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.May 23, 2001 · N16895 · Doug DC982SDR DL757010797Radome · damagedCREW REPORTED RADAR FAILED AT FL240. ON ARR PBI GROUND CREW NOTICED RADOME UPPER LEFT CRUSHED IN. AN AREA ABOUT THE SIZE OF THREE BASKET BALLS. THE RADOME WAS REPLACED, AND THE RADAR ANTENNA ALSO AS A PRECAUTION. INSPECTED NOSE BULKHEAD AND A/C, NO OTHER DMay 18, 2001 · N631DL · Boeing 757232SDR C1HA200196003Plate · looseAT FL 290 AIRSPEED ABOVE 290KTS AIRFRAME HAS INTERMITTANT STRONG VIBRATION DOES NOT CHANGE WITH POWER SETTINGS. INSPECTED AIRCRAFT AND FOUND LOOSE BODY TO WING FAIRING SEAL GUIDE PLATE. TIGHTENED AS REQUIRED. TEST FLEW A/C, NO DEFECTS NOTED.May 4, 2001 · N696CA · Boeing 7272J4SDR RRXA011043Fairing · damagedAFTER OFF LOAD, DISCOVERED DAMAGE TO ACFT WING/FUSELAGE FAIRING APPROX 30 INCHES FWD OF CENTER CARGO DOOR FWD EDGE. REPAIRED DAMAGED FORMED ANGLE COMMON TO THE WING/FUSELAGE FAIRING AT AREA NOTED AS PER GUIDELINES IN THE DC-10 SRM CHAPTER 51 STANDARD PRACTICEMay 3, 2001 · N47816 · Doug DC1030FSDR ZW0A0100102Bracket · crackedDURING CHECK-C MAINT ON RT WING L/E THE INBD L/E FAIRING ATTACH BRACKETS WERE CRACKED, INBD OF ZERO L/E SLAT. REMOVED 2 BROKEN BRACKETS. FABRICATED NEW BRACKETS PER DRAWING 5937452 AND SRM 51-30-5. INSTALLED PER SPM 6-70-01. TREATED AND PAINTED PER SRM 51-Apr 4, 2001 · N909TW · Doug DC982SDR C2XA01TY065Skin · nickedTYS DURING A SCHEDULED INSPECTION THE TAIL CONE WAS FOUND TO BE NICKED BEYOND MANUFACTURES LIMITS. MAINTENANCE REPAIRED THE TAIL CONE IAW EMB GST-0994/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIONApr 1, 2001 · N15980 · Emb EMB145LRSDR ASAA0180124Wire Rope · out of positionPDX - DURING SERVICE CHECK, FOUND TAILCONE RELEASE CABLE OFF ONE OF THE CAMS. PROPERLY LOOPED RELEASE CABLE OVER CAM. (M)Mar 31, 2001 · N958AS · Doug DC983SDR UPS01235493Frame · corrodedINSPECTION TYPE: C & SI, LT WING TO BODY FAIRING NR 3335 HAS CORRODED FRAME. RIVETS REMOVED FROM CORRODED FRAME IAW SRM 51-30-2 CORRODED FRAME CUT OUT IAW SRM 51-10-6 REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1Mar 23, 2001 · N926UP · Boeing 72731CSDR DHL2001806508Fairing · crackedC-CHECK.- LT WING TO FUSELAGE FAIRING SUPPORT ANGLE CRACKED 3/4 INCH AT STA. 640 L-21LT. TO L-22 LT. REMOVED FAIRING SUPPORT ANGLE IAW SRM.51-1-21 PAGE 1 FABRICATED ANGLE IAW. SRM 53-2-0 FIG 1B CLEANED,TREATED & PRIMED IAW SRM 51-1-8B INSTALLED ANGLE IAW.SRM Mar 7, 2001 · N806DH · Doug DC873FSDR AWXA0001482Radome · puncturedLAS - 3/5/01 - ON DESCENT INTO LAS PASSING THROUGH 18,000 FT THE CREW HEARD A LOUD BANG AND AIR RUSHING SOUND FROM THE NOSE AREA AND FELT VIBRATION IN THE FLOOR. AN UNEVENTFUL LANDING WAS MADE IN LAS. UPON INSPECTION THE RADOME WAS FOUND TO HAVE A LARGE DENTMar 7, 2001 · N907AW · Boeing 757225SDR GTIA010047Tail Cone · dislodgedMYR - FLT 303 - TAILCONE CAME OFF ON LANDING. TAILCONE RELEASE SYSTEM EVACUATED AND REPAIRED BY BOEING. REPLACED EXTERIOR CABLE FITTING AND RIGHT LOWER LOCKING PIN. TAILCONE WAS FIT FOR CLEARANCES AND DROP CHECK PERFORMED AS PER DC-9 MM 53-50-3. (M)Feb 24, 2001 · N130NK · Doug DC941SDR 2001UALA00161Screw · missingDIVERTED DUE TO A PASSENGER SEEING A SCREW FALL OUT OF THE ENGINE MOUNT AREA. *S/D* FOUND FAIRING WITH MISSING SCREW. REPLACED SCREW.Feb 24, 2001 · N307UA · Boeing 737322SDR GTIA010043Tail Cone · separatedDCA - FLT 72 - TAILCONE FELL OFF DURING LANDING. REMOVED AND REPLACED TAILCONE IAW MM 53-50-3, OPS CHECK NORMAL. (M)Feb 23, 2001 · N130NK · Doug DC941SDR F3LA200100034Fairing · damagedAIRCRAFT DIVERTED TO GRAND JUNCTION, COLORADO DUE TO WEATHER. UPON WALKAROUND, FLIGHT CREW REPORTED DAMAGE TO RT INBD WING-TO-BODY FAIRING ELEPHANT EAR SCUFF PLATES DAMAGED. AIRCRAFT WAS FERRIED TO DEN FOR REPAIR. MAINTENANCE REPLACED RT INBD WING-TO-BODY FFeb 23, 2001 · N270FL · Boeing 7372L9SDR UPS01835034Fairing · crackedINSPECTION TYPE:N/A, LEFT (CENTER FUESLAGE) PANEL CRACKED AND DELAMINATED JUST FWD OF LEFT MAIN GEAR DOOR. REMOVED PANEL. *S/D* REINSTALLED SERVICEABLE ADF PANEL PER 34-51-01.Feb 22, 2001 · N804UP · Doug DC873FSDR MWEA010161Clip · brokenTAIL CONE AFT INTERIOR HANDLE HAS A BROKEN CLIP AND FAILS PULL CHECK (25 - 35 LBS). REMOVED AND REPLACED CLIP.Feb 19, 2001 · N212ME · Doug DC932SDR ASAA0180075Cable · disconnectedSEA - DURING LANDING, ''TAILCONE MISSING'' ANNUNCIATOR ILLUMINATED. SUBSEQUENT INSPECTION REVEALED THE EXTERNAL RELEASE HANDLE CABLE HAD BECOME DISCONNECTED. RECONNECTED RELEASE CABLE PER MM 53-50-00. (M)Feb 18, 2001 · N951AS · Doug DC982SDR DHL200171208CAngle · crackedAT C-CK; RT WING FAIRING SUPPORT ANGLE CRACKED .5 INCH AT STA 330.000. PERFORMED STOP DRILL IAW SRM 51-10-1, PG 6B, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-10-2, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-40, PG 1-2.Jan 30, 2001 · N712DH · Boeing 72729
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