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 200800305Skin · scratchedUPPER WING TO BODY FAIRING, FROM STA 620 TO STA 1000 FROM STR 23R TO STR 34R HAS SCRIBE MARKS. APPROX STA 670 STR 31R .005 DEPTH. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .005 WITHIN LIMITS, ALODINED AND PRIMED AREA PER B747 SP SRM'S 53-31-00 PG 1-4, 51-Mar 17, 2008 · N708BA · Boeing 747SPB5SDR UPS08851877Skin · crackedINSPECTION TYPE:N/A CRACK AND CORROSION ON TAIL CONE UPPER SURFACE. C/O DAMAGE AND RADIUSED 4 EA CORNERS. DAMAGE REMOVED. FABRICATED PARTS FILLER & DOUBLER, OK TO INSTALL PER QC. INSTALLED REPAIR. ITEM 371453 ASSIGNED FOR 6000 CYCLES PER DC8 SRM 53-02-01Mar 16, 2008 · N811UP · Doug DC873FSDR VNAA0803007Radome · damagedCREW REPORTED ON APPROACH A LIGHTNING STRIKE TO THE NOSE AREA. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RADOME AND OTHER AREAS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THEMar 15, 2008 · N206PS · Cndair CL6002B19SDR 08FDEA00936Skin · delaminatedDELAMINATION ON PANEL NR 143 FL; INTERIOR SKIN. REPAIRED IAW SRM 51-77-10 & 51-75-10.Mar 14, 2008 · N425FE · Airbus A310203SDR 08FDEA00935Fairing · puncturedPUNCTURE ON THE INTERIOR SURFACE OF PANEL NR 144FR. REPAIRED INTEROR SURFACE OF PANEL 144 FR BY REMOVING THE DAMAGE. CLEANED & PREPPED FOR APPLICATION OF THE WET LAY UP. APPLIED, CURED & SANDED THE WET LAY UP. CLEANED & PREPPED FOR THE APPLICATION OF THE REMar 14, 2008 · N425FE · Airbus A310203SDR COMA0860167Sealant · missingFLIGHT 5451 - UPON FLAP SELECTION TO 8 DEGREES A THUMPING WAS FELT. ABORTED APPROACH, DECLARED EMERGENCY, TOWER VERIFIED GEAR DOWN UPON SELECTION. LANDED WITHOUT INCIDENT. REPLACED MISSING SEALANT TO BELLY AND WING ROOT FAIRINGS. NO FURTHER DEFECTS.Mar 10, 2008 · N933CA · Cndair CL6002B19SDR HNAA0800100Radome · damagedENCOUNTERED LIGHTNING STRIKE, INFLIGHT SYSTEM CHECK GOOD. INSPECTED AIRCRAFT, EVIDENCE OF BURN MARKS ON RIGHT HAND SIDE OF RADOME, WILL FERRY AIRCRAFT TO ROA. REMOVED AND REPLACED RADOME.Mar 7, 2008 · N327EN · Dhav DHC8311SDR 08FDEA00783Frame · corrodedBODY TO WING FAIRING PANEL, NR 3218 BETWEEN PRIMARY HEAT EXCHANGER RT O/B FRAME WEB HAS CORROSION ON MATING SURFACE AT FS 825, RBL WL 138. RT O/B FRAME WEB FOUND TO HAVE 50 PERCENT MATERIAL LOSS, OUT OF LIMITS REF SRM 51-10-01. REMOVED AND REPLACED FRAME WEBMar 7, 2008 · N486FE · Boeing 727227SDR 08FDEA00729Panel · damagedRT FUSELAGE, TO WING FILLET PANEL 152GT HAS A CHUNK OUT OF THE LOWER EDGE. REMOVED DAMAGED, CLEANED & PREPPED REPAIR. APPLIED REPAIR PLYS & VAC BAGGED. CURED & SANDED. APPLIED FIBERGLASS SEALER, CURED & SANDED SMOOTH IAW SRM 51-43-01 VOL II PARA 16-A (4)Mar 5, 2008 · N384FE · Doug MD1010FSDR 08FDEA00716Fillet · puncturedLT FILLET PANEL NR 577BL IS PUNCTURED. REPAIRED PUNCTURES IAW SRM 51-77-12.Mar 5, 2008 · N425FE · Airbus A310203SDR M7K2008F00131Fitting · crackedDURING ROUTINE 100 HOUR INSPECTION, A CRACK WAS FOUND RADIATING ACROSS THE CORNER OF THE FIRST HOLE ON THE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL ON THE FAIRING ATTACHMENT FLANGE. A NEW PART WAS INSTALLED IAW THE REQUIREMENTS OF AD2004-01Mar 3, 2008 · N807MH · Urocop EC130B4SDR FDKA200802062Attach Angle · crackedTHE ATTACH ANGLE FOR THE LT WING TO FUSELAGE FAIRING IS CRACKED, JUST AFT OF THE CENTER WING. THE DAMAGE HAS BEEN REPAIRED.Feb 14, 2008 · N836MJ · Emb EMB145LRSDR UIEA200800042Radome · damagedAIRCRAFT WAS HIT BY LIGHTNING STRIKE. ENTRANCE AT THE RADOME. NO COMMUNICATIONS OR NAV FAILURES REPORTED BY CREW. FOUND RADOME DAMAGED BY LIGHTNING STRIKE. FOUND RIGHT HF ANTENNA DAMAGED BY LIGHTNING STRIKE. LIGHTNING STRIKE INSPECTION ACCOMPLISHED PER 5-Feb 13, 2008 · N528MC · Boeing 7472D7BSDR G60A200800028Tail Cone · crackedTAILCONE CRACKED APPROX 1 INCH AT UPPER RT SIDE IN WEB.Feb 8, 2008 · N607GC · Doug DC1030FSDR A6WA200840089Radome · crackedLIGHT GLAZING ON RADOME FOUND CRACK. (K) REPLACED IAW SRM 51-42-20. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19SDR CA080122003Structure · cracked(CAN) WHILE INSPECTING SOME ITEMS, MFG CONTINUED AIRWORTHINESS PROGRAM IT WAS NOTICED THAT 2 CRACKS CAME FROM THE RUDDER CABLE HOLES AND ANOTHER CRACK CAME FROM THE NUTPLATE UNDER THE DOUBLER. CONTINUED AIRWORTHINESS INSP 53-40-04 COVERS THIS INSPECTION BUT ISJan 21, 2008 · Cessna U206GSDR 08FDEA00492Strut · corrodedTAIL CONE, SMALL SPOTS OF CORROSION AT LT AFT TRACK ATTACHMENT FITTING AT FRAME 87. STRUT-CROSS WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.Jan 21, 2008 · N447FE · Airbus A310222SDR 08FDEA00491Strut · corrodedTAIL CONE, SMALL SPOTS OF CORROSION AT TRACK LT, ATTACHMENT FITTING TO FR 86. STRUT-CROSS WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.Jan 17, 2008 · N447FE · Airbus A310222SDR 08FDEA00490Strut · corrodedTAIL CONE, SMALL SPOTS OF CORROSION AT TRACK LT, ATTACHMENT FITTING TO FR 86, STRUT-CROSS WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.Jan 17, 2008 · N447FE · Airbus A310222SDR 08FDEA00489Rib · damagedTAIL CONE, RIBS BETWEEN FR 84 AND 86, AND STRINGER 32 LT DAMAGED, RIBS (SECTION-L) WERE REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.Jan 17, 2008 · N447FE · Airbus A310222SDR 08FDEA00488Rib · damagedTAIL CONE, RIBS BETWEEN FRAME 85 TO 87 AND STRINGER 33 RT DAMAGED. THE RIBS (SECTION-L) WERE REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.Jan 17, 2008 · N447FE · Airbus A310222SDR UPS08851704Frame · corrodedINSPECTION TYPE:C2 TAIL CONE FRAME FWD OF LOWER NAV LIGHT CUTOUT HAS CORROSION. REPAIRED TAIL CONE FRAME FWD OF NAV LIGHT IAW RAA DC8-53-20678 AND EA 008-5710-01-A1261.Jan 10, 2008 · N702UP · Doug DC871FSDR C2XA08TY005Fairing · damagedLEFT WING TO FUSELAGE FAIRING 193 GROUND DAMAGE REPAIR. PERFORMED PLY RESTORATION TO EACH SKIN, ONE AT A TIME INCLUDING CORE REPLACEMENT. EXPOXY PRIME AND FINISH PAINT REPAIR. REPAIR ACCOMPLISHED IAW EC5350-01104. EMB IC2008-145/00110; ENGINEERING PROJECT Jan 8, 2008 · N27506 · Emb EMB135ERSDR MALA070199Skin · dentedDENT LOCATED IN RT UPPER TAILCONE SKIN AT FS827 WITH DEFORMED FRAME. INSTALLED FRAME REINFORCEMENT IAW MAL EO NR S53509.Dec 21, 2007 · N418XJ · Saab 340BSDR F3LA200700393Fastener · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORRODED FASTENERS THAT SECURE LIGHT TO RT WING-TO-BODY FAIRING 192DT. REMOVED AND REPLACED RT UPPER WING LIGHT COVER MOUNTING SCREWS ON PANEL NR 192DT.Dec 20, 2007 · N912FR · Airbus A319111SDR F3LA200700392Fastener · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED RT WING-TO-BODY FAIRING 192DT HAD CORRODED FASTENERS AT LOWER SEAL. REMOVED AND REPLACED RT WING UPPER WING-TOO-BODY FAIRING PANEL NR 192DT LOWER SEAL MOUNTING SCREWS IAW 51-42-11.Dec 20, 2007 · N912FR · Airbus A319111SDR LR7A07131Fairing · warpedDURING SCHEDULED C-3 CHECK, PER JOB CARD HC5301 FOUND RAMP DOOR EXTERIOR LT SIDE PEDESTAL FAIRING SKIN WARP FS 845 (RAMP STA 10) LBL24. REPAIR ACCOMPLISHED BY REPLACING FAIRING SKIN IAW SMP583 CHAPTER 51-60 AND 51-70.Dec 19, 2007 · N406LC · Lkheed 382GSDR LR7A07130Fairing · warpedDURING SCHEDULED C-3 CHECK, PER JOB CARD HC5301 FOUND RAMP DOOR EXTERIOR FWD PEDESTAL FAIRING SKIN WARP AT FS 845 (RAMP STA 10). REPAIR ACCOMPLISHED BY REPLACING FWD FAIRING IAW SMP583 CHAPTER 51-60 AND 51-70.Dec 19, 2007 · N406LC · Lkheed 382GSDR 07FDEA04824Frame · corrodedBODY FAIRING FRAME LOCATED BETWEEN PANELS 3358 AND 3458, FORWARD END HAS CORROSION. REPLACED FAIRING FRAME, REF BOEING DWG 65-59318 AND SRM 51-30-2, TREATED AND PRIMED REF MM 51-20-021-7, THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 17, 2007 · N464FE · Boeing 727225SDR HEER118215Angle · crackedFWD LT CAP ANGLE CRACKED. REPORTED PROBLEM TO MFG.Nov 16, 2007 · N192PH · Skrsky S92ASDR WRLA2007127Support Beam · corrodedDURING C-CHECK INSPECTION CORROSION FOUND RT WING TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z=-20. REPAIRED THE RT WING TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z-20 PER SRM VOL 1 53-00-01 FIG 9 REV 40. REF EGAT NRC U05030.Nov 10, 2007 · N278WA · Doug MD11SDR LR7A07122Skin · crackedDURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND RT BOTTOM WHEEL WELL FAIRING SKIN CRACKED AT BELLY ATTACHMENT AREA FS 537 & FS 577, WL 132, RBL 45. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 USING 2024T3 .040".Nov 6, 2007 · N401LC · Lkheed 382GSDR LR7A07121Skin · crackedDURING SCHEDULED B-2 CHECK PER JOB CARD HB5301 FOUND LT BOTTOM WHEEL WELL FAIRING SKIN CRACKED AT BELLY ATTACH POINT, FS 517, WL 130, LBL 45. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 USING 2024T3 .040".Nov 6, 2007 · N401LC · Lkheed 382GSDR CA071031006Radome · damaged(CAN) FLIGHT ON CLIMB OUT THE CREW HEARD A LOUD BANG IN THE NOSE AND SAW A BIRD TRAVEL PAST THE COCKPIT WINDOW. ALL FLIGHT SYSTEMS WERE NORMAL AND FLIGHT CONTINUED. UPON ARRIVAL MAINTENANCE MET THE AIRCRAFT AND FOUND A HOLE IN THE RADOME AS WELL AS A DAMAGE TOOct 30, 2007 · Cndair CL6002B19SDR A6WA200740596Seal · missingDURING CRUISE INTERMITTENT VIBRATION AT 280 KNOT FOR APPROX 5 SECONDS. ALL ENGINE PARAMETERS WERE NORMAL. APPLIED SEALANT TO WING TO FUSELAGE FAIRING AS REQUIRED IAW CRJ AMM 51-23-00 AS REQUIRED. (M)Oct 30, 2007 · N411ZW · Cndair CL6002B19SDR TRAX200701594Skin · corrodedON MLG SKIN CORRODED AT FR 27 BL 0. CORROSION REMOVED ON MLG SKIN AT FR 27 BL 0 IAW SRM 51-21-42 U/T PERFORMED IAW NTM NOM=0.063" MIN=0.060". REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IOct 25, 2007 · N643AS · Aerosp ATR72SDR USAA920071019Bracket · corrodedBFM - MAJOR REPAIR - C2 CHECK, CORROSION ON BODY FAIRING SUPPORT STRUCTURE BRACKET, BS 2948 / FR 39.2. REPLACED BODY FAIRING SUPPORT STRUCTURE BRACKET, BS 2948 / FR 39.2 IAW A330 SRM 53-35-14 AND 51-42-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOOct 19, 2007 · N274AY · Airbus A330323SDR USAA920071018Web · crackedBFM - MAJOR REPAIR - C2 CHECK - CRACK ON AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, -Y2820, WL -Z1650. REPAIRED AFT BELLY FAIRING SUPPORT STRUCTURE WEB 3990 / FR 53.2, -Y2820, WL -Z1650 I/A/W A330 SRM 53-35-14 AND 51-44-11. AIRCRAFT MANUFACTOct 17, 2007 · N274AY · Airbus A330323SDR USAA920071017Web · crackedBFM - MAJOR REPAIR - C2 CHECK - CRACK ON AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, +Y2820, WL -Z1650. REPAIRED AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, +Y2820, WL -Z1650 IAW A330 SRM 53-35-14. AIRCRAFT MANUFACTURER AND MOOct 17, 2007 · N274AY · Airbus A330323SDR U5QA06007Seal · looseCREW REPORTED STRANGE NOISE FROM RIGHT SIDE OF FUSELAGE DURING CLIMB. SOUNDED LIKE SOMETHING VIBRATING AGAINST THE OUTSIDE OF FUSELAGE JUST ABOVE THE WING. AFTER LANDING THE CREW REPORTED THAT THE WING TO FUSELAGE RUBBER SEAL HAD COME LOOSE AT THE TRAILING EOct 10, 2007 · N903SC · Hawker BAE125700BSDR DLM88071464Structure · crackedCRACKED LOWER TAIL CONE STRUCTURE. REPAIRED PER SRM 51-90-0D.Oct 8, 2007 · N953DL · Doug MD88SDR MWEA070240Skin · peelingFUSELAGE AT STATION 37 RADOME HINGE AREA SKIN PEELED UP AT RADOME HINGE POINT. FABRICATED AND INSTALLED DOUBLER.Oct 5, 2007 · N814ME · Doug DC981SDR MWEA070238Radome · crackedCRACK FOUND AT LEFT RADOME HINGE FASTENER. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER.Oct 5, 2007 · N814ME · Doug DC981SDR 2007FA0001083Tail Cone · crackedFOUND CRACK DURING ROUTINE 2,3,D PHASE INSPECTION. (K)Sep 27, 2007 · N731BH · Cessna 441SDR UIEA200700445Fairing · delaminatedFUSELAGE FAIRING 193C AREA OF DELAMINATION. DELAMINATED AREA REPAIRED AS PER SRM 51-40-12Sep 26, 2007 · N809MC · Boeing 747228FSDR 2007FA0000849Fairing · separatedLOWER SECTION OF RT WING ROOT FAIRING SEPARATED FROM AIRCRAFT IN FLIGHT. FAIRING IS RETAINED WITH JUST A FEW SCREWS AND AN AREA OF THE LOWER PORTION OF FAIRING IS RETAINED WITH DOUBLE SIDED TAPE AND AN AREA OF DOUBLE SIDED TAPE CAME DEBONDED AND AIR GOT UNDERSep 26, 2007 · N631SR · Cirrus SR22SDR ASMF200709002Radome · damagedAIRCRAFT WAS HIT BY A STAIR THAT GOT MOVED BY A STRONG WIND DURING A STORM, RESULTING DAMAGE ON RADOME RT FRONT SIDE OF 23 INCH LENGTH WITH 5 PERFORATIONS (2 IN LOWER EXTREME AND 3 IN UPPER EXTREME) AND EXPOSITION OF COMPOUND MATERIAL. THE DETAILS OF THE REPAISep 4, 2007 · N850AM · Boeing 737*SDR UPS07850723Frame · corrodedINSPECTION TYPE:C2 TAIL CONE LWR NAV LIGHT LENS FWD FRAME HEAVILY CORRODED AT STA 1973. REPAIRED TAIL CONE LOWER NAV LIGHT LENS FORWARD FRAME IAW SRM 51-01- 04, DWG 5704663-3, SRM 53-05-03, SRM 51-1-8 AND SRM 51-1-21.Aug 31, 2007 · N801UP · Doug DC873FSDR MWEA070202Panel · inoperativeTAIL CONE EXIT DOOR ARM/DISARM PANEL DOES NOT STAY IN DISARMED POSTION OR DOES NOT LATCH PROPERLY. RESECURED PANEL.Aug 30, 2007 · N813ME · Doug DC981SDR DHL2007785006Radome · crackedAT COMPLETION OF PUSH BACK, GROUND CREW UNABLE TO REMOVE TOW BAR. WHEN TOW BAR RELEASED, WITH PARKING BRAKE SET, ACFT MOVED FORWARD. VISIBLE DAMAGE NOTED TO RADOME ASSY.Aug 25, 2007 · N785AT · Boeing 727214
Back to JASC 5350