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 DALA14021070915Release Cable · damagedMAINTENANCE DISCOVERED THAT THE INSULATION ON THE LT RELEASE LATCH CABLE FOR THE TAILCONE WAS DAMAGED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPAIRED IAW ER/A 523964-14 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTApr 5, 2014 · N915DL · Doug MD88SDR SWIA201437979Structure · corrodedAFT SUPPORT STRUCTURE FOR WING TO BODY FAIRING IS CORRODED ON CENTER FWD HYDRAULIC ACCESS PANEL LANDING AT FS 847 OUT OF LIMITS. C-CHECK, R & R AFT SUPPORT STRUCTURE FOR WING TO BODY FAIRING FS 847 FWD HYDRAULIC ACCESS PANEL LANDING IAW SRM.Apr 4, 2014 · N227AG · Cndair CL6002C10SDR AALA20140404007Attach Angle · corrodedBS 1020 RT WING UPPER WING TO BODY PANEL ATTACH ANGLE CORRODED. R & R FILLER IAW AARD 51-20-00-1.Apr 4, 2014 · N656AA · Boeing 757223SDR DALA14020430935Striker · out of positionPERFORMED TAILCONE RELEASE SYSTEM OPS CHECK, SYS FAILED, AND MAINTENANCE FOUND THE TAILCONE EXTERIOR RELEASE CABLE PULL FORCE WAS OUT OF ALLOWABLE LIMITS. FOUND WAS THE DOOR JAMB UPPER FITTING WAS OUT OF CONFIGURATION AND WAS CORRECTED BY REMOVING THE STRIKERApr 3, 2014 · N935DL · Doug MD88SDR DALA14020330935Pulley · wornMAINTENANCE DISCOVERED THAT THE INBD RELEASE LATCH CABLE PULLEY FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE PULLEY WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Apr 1, 2014 · N935DL · Doug MD88SDR DALA14020290915Cable · frayedMAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.Mar 31, 2014 · N915DL · Doug MD88SDR DALA14020230935Bracket · wornMAINTENANCE DISCOVERED THAT THE KEVLAR CABLE CAM BASE BRACKET FOR THE TAILCONE WAS WORN, OUT OF ALLOWABLE LIMITS. THE KEVLAR CABLE CAM BASE BRACKET WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Mar 29, 2014 · N935DL · Doug MD88SDR SWAA2014041727202Panel · crackedFAIRING 191D CRACKED OUT FASTENER HOLE ON FWD EDGE. REPAIRED PANEL IAW SRM.Mar 25, 2014 · N425LV · Boeing 7377H4SDR SIMA20140318009Attach Angle · crackedDURING HMBV INSPECTION FOUND RT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE IS CRACKED BETWEEN FRAMES 47 - 48. CRACK APPROXIMATELY 1 INCH LONG. INSTALLED NEW ANGLE IAW SRM CH 51-40-02.Mar 18, 2014 · N636AE · Emb EMB145LRSDR SIMA20140318010Attach Angle · crackedDURING HMBV INSPECTION FOUND LT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE IS CRACKED BETWEEN FRAMES 45 - 46 & AT FRAME 46. THIS REPAIR IS LOCATED ON THE SAME ANGLE & IS FARTHER AFT THAN THE CRACK AT FRAME 45 - 46. IAW NRWC E374048 FOR THE AFT SECTION OF THMar 18, 2014 · N636AE · Emb EMB145LRSDR DALA14017620961Cam · wornDURING A CHECK OF TAILCONE, MAINTENANCE FOUND THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.Mar 18, 2014 · N961DL · Doug MD88SDR AALA20140318007Pin · crackedCRACK AT RADOME GUIDE PIN AT STATION 37, 6 O`CLOCK POSITION. STOP DRILLED CRACK & INSTALLED DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET 3.Mar 18, 2014 · N590AA · Doug DC983SDR SWAA2014041427054Support Angle · crackedUNDER WING TO BODY FAIRING SUPPORT ANGLE CRACKED BETWEEN BS 520 TO BS 540+11, STRINGER 22R. REPAIRED ANGLES IAW EO & EA.Mar 16, 2014 · N353SW · Boeing 7373H4SDR SIMA20140312019Attach Angle · crackedRIGHT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE IS CRACKED AT FRAME 47 CRACK APPROXIMATELY 1 INCH LONG. INSTALLED NEW ANGLE IAW SRM CH 51-40-02.Mar 12, 2014 · N636AE · Emb EMB145LRSDR SWAA2014041427050Angle · crackedWING TO BODY FAIRING INTERNAL AREA ANGLE CRACKED AT BS 540, STRINGER 22R. REPAIRED ANGLE IAW EA.Mar 9, 2014 · N353SW · Boeing 7373H4SDR SWAA2014040926948Support Angle · crackedLEFT FWD WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT BS 540. R & R ANGLE IAW SRM & DWG.Mar 9, 2014 · N353SW · Boeing 7373H4SDR SWAA2014040826937Drag Angle · crackedWING TO BODY FAIRING INTERNAL AREA DRAG ANGLE CRACKED AT BS 540, STRINGER 22R. REPAIRED ANGLE IAW SRM.Mar 9, 2014 · N353SW · Boeing 7373H4SDR SIMA20140305025Support Bracket · crackedRIGHT OVERWING FAIRING UPPER ATTACHMENT FLANGE SUPPORT BRACKET BETWEEN FRAME 48 & 49 CRACKED. R & R RT OVERWING FAIRING UPPER ATTACHMENT FLANGE SUPPORT BRACKET BETWEEN FRAME 48 & 49 IAW SRM 51-40-02.Mar 5, 2014 · N639AE · Emb EMB145LRSDR DALA14021060960Release Cable · damagedMAINTENANCE DISCOVERED THAT THE INSULATION ON THE LT RELEASE LATCH CABLE FOR THE TAILCONE WAS DAMAGED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPAIRED IAW ER/A 523964-14 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTMar 5, 2014 · N960DL · Doug MD88SDR SWAA2014030425728Support Bracket · corrodedLT WING TO BODY SUPPORT BRACKET CORRODED BETWEEN BS 832 TO BS 847, LONGERON 30L. R & R FORMER IAW SRM.Feb 26, 2014 · N939AT · Boeing 717200SDR R61A201402200331Fairing · damagedDURING HEAVY CHECK, LT SIDE SKIRT FAIRING AT SPLICE FOR UPPER 195 FAIRING PANEL FWD EDGE FOUND TO HAVE CRACKED AND DAMAGED RIVETS. MX REPAIRED DAMAGE SKIRT FAIRING IAW ETD 2014-170-015453.Feb 20, 2014 · N803MD · Emb ERJ170100SUSDR DALA14011499007Release Cable · looseTHE CAPTAIN REPORTED THAT THE OVERHEAD WARNING ALERTED FOR THE TAILCONE NOT BEING SECURED. MAINTENANCE FOUND THAT THE TAILCONE RELEASE SYSTEM CABLE WAS LOOSE AND REQUIRED REPLACEMENT. CABLE REPLACED AND SYSTEM RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPFeb 20, 2014 · N907DE · Doug MD88SDR DALA14010520987Bracket · looseDURING CHECK, NOTED THE LOWER ATTACH BRACKET FOR THE TAILCONE UPPER LT LOCK RECEPTICLE PAD WAS LOOSE AND WORKING. REPLACED TAILCONE BRACKET IAW SRM 53-30-01.Feb 18, 2014 · N987DL · Doug MD88SDR DALA14010540987Cable · frayedDURING CHECK, NOTED THE TAILCONE KEVLAR CABLE WAS FRAYED AND DETERIORATED. REPLACED KEVLAR CABLE IAW AMDS 5350-01077-0101.Feb 16, 2014 · N987DL · Doug MD88SDR DALA14010530987Receptacle · wornDURING CHECK, NOTED THE PIN RECEPTICLES ON THE TAILCONE ARE WORN. REPLACED TAILCONE RECEPTICLES IAW SRM 51-30.Feb 16, 2014 · N987DL · Doug MD88SDR DALA14009640904Structure · corrodedMAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE HAD CORRODED HARDWARE. THE CLIPS WERE REPLACED, ADJUSTED, AND THE RII WAS SATISFACTORY.Feb 13, 2014 · N904DL · Doug MD88SDR CALA2014021390375Frame · tornFAIRING FRAME ASSEMBLY AT BS 900, LBL 12 IS TORN, IAW SRM 53-30-71 PG2. REPAIRED IAW ECRA 5352-01080 & 5342-01094.Feb 12, 2014 · N509UA · Boeing 757222SDR CALA2014021390373Frame · damagedDAMAGE TO FAIRING FRAME ASSEMBLY AT BS 900. ACCOMPLISHED RII REQUIREMENT OF SMC15, CHECK ACCOMPLISHED.Feb 12, 2014 · N509UA · Boeing 757222SDR DALA14009660904Bracket · wornMAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE SYSTEM LATCH CABLE SAFETY PIN HOLE WAS WORN OUT OF ALLOWABLE LIMITS, IN THE PULLEY BRACKET. LOCATED ON THE LT 8:30 POSITION. BRACKET REPLACED AND RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.Feb 12, 2014 · N904DL · Doug MD88SDR DALA14009650904Bracket · wornMAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE SYSTEM LATCH CABLE SAFETY PIN HOLE WAS WORN OUT OF ALLOWABLE LIMITS, IN THE PULLEY BRACKET. LOCATED ON THE LT 9:00 O`CLOCK POSITION. BRACKET REPLACED AND RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETEDFeb 12, 2014 · N904DL · Doug MD88SDR CALA2014021290366Seal · out of positionVIBRATION AFTER TAKEOFF. CREW FELT AIRFRAME VIBRATION STRONG ON TO THRU 5500 FEET WHEN IT DISSIPATED. CABIN CREW ALSO FELT THE SAME VIBRATION ON FINAL APPROACH, VIBRATION RETURNED IN THE AFT CABIN. FOUND SEAL AT PANEL 191DL NOT FLUSH WITH WING UPPER SURFACEFeb 11, 2014 · N544UA · Boeing 757222SDR COEA2014040443908Angle · corrodedHEAVY CHECK COE. DORSAL PANEL MOUNTING ANGLES ARE CORRODED, FWD OF PANEL 321AL. BOTH ANGLES WERE REPLACED WITH NEW PARTS IAW ATR42 SRM.Feb 9, 2014 · N908FX · Aerosp ATR42300SDR CALA2014021090340Fairing · unsecureLOUD HUMMING SOUND AROUND ROW 22. INSPECTED SEALS ON BOTH LT & RT SIDE, NO DEFECTS FOUND. TAPED FAIRINGS 191DT & 192DT. CREW ON FLIGHT 330 7 REPORTED NO HUMMING.Feb 7, 2014 · N483UA · Airbus A320232SDR SWAA2014021125054Angle · crackedLT WING TO BODY FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.Feb 3, 2014 · N952AT · Boeing 717200SDR SWIA201436375Channel · crackedAFT BELLY FAIRING PANEL 196DR HAS CRACKED C CHANNEL. C-CHECK REPLACED C CHANNEL ON AFT BELLY FAIRING PANEL 196DR, PN CC670-39251-1 IAW MODSUM.Feb 1, 2014 · N766SK · Cndair CL6002C10SDR DALA14006519529Tail Cone · no testDURING ROUTINE TAILCONE DROP IAW TASK 95-0552-8-0001, THE TAILCONE WOULD NOT DEPLOY. COMPLIED WITH REPAIRS IAW ER/A 95-522520-14 AND THE TAIL CONE LOCK MECHANISIM WORKED CORRECTLY WHILE ACCOMPLISHING TAIL CONE OPS CHECK.Jan 29, 2014 · N991AT · Boeing 717200SDR DALA14006160933Receptacle · wornMAINTENANCE DISCOVERED THAT BOTH THE LT UPPER AND THE RT UPPER RELEASE SPADE RECEPTACLE FOR THE TAILCONE WERE WORN OUT OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORIJan 28, 2014 · N933DL · Doug MD88SDR DALA14006150933Cam · damagedMAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS MISSING HARDWARE; WHICH CAUSED IT TO BE OUT OF ALLOWABLE RIG LIMITS, EXCESSIVE FORE & AFT PLAY. THE CAM BASE WAS REPLACED AND MISSING SPACERS/SHIMS WERE THEN INSTALLED. THE SYSTEM WAS RIJan 28, 2014 · N933DL · Doug MD88SDR DALA14006429235Release Cable · frayedTAILCONE RELEASE BOTTLE ATTACH CABLE FRAYED. R & R TAILCONE RELEASE BOTTLE CABLE IAW AMM.Jan 27, 2014 · N935DN · Doug MD9030SDR DALA14006359235Guide · damagedDURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE EXTERIOR EMREGENCY EXIT PULL HANDLE ANGLE BROKEN. R & R ANGLE GUIDE ON TAILCONE EXTERIOR EMERGENCY EXIT PULL HANDLE. OPS CHECKED GOOD IAW AMDS 5352-7116, STEP 5, A-1-A.Jan 27, 2014 · N935DN · Doug MD9030SDR DALA14005569235Handle · brokenEXTERIOR TAILCONE PULL RELEASE HANDLE BROKEN. REPAIR ACCOMPLISHED ON NR 124.Jan 26, 2014 · N935DN · Doug MD9030SDR CA140124007Fairing · ruptured(CAN) DURING WALK AROUND INSPECTION, IT WAS FOUND THAT THE RT VERTICAL STABILIZER TO FUSELAGE FAIRING WAS DAMAGED, REFER IPC 53-19-69, ITEM 250. AFTER INSPECTION IT WAS NOTED THAT THE DAMAGE WAS DUE TO DELAMINATION OF THE PANEL. PANEL REPLACED AND INFORMED.Jan 23, 2014 · Airbus A310300SDR DALA14005349236Release Cable · frayedDURING SERVICE CHECK, FOUND TAILCONE RELEASE CABLE FRAYED. R & R CABLE IAW AMM. RIGGED IAW AMM.Jan 23, 2014 · N936DN · Doug MD9030SDR DALA14005160932Bracket · wornMAINTENANCE DISCOVERED THAT THE TAILCONE LT AND RT SPRING BRACKETS ARE WORN BEYOND 50 PERCENT. BRACKETS REPLACED AND SYSTEM RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK COMPLETED SATISFACTORILY.Jan 23, 2014 · N932DL · Doug MD88SDR DALA14005150932Conduit · out of positionMAINTENANCE DISCOVERED THAT THE TAILCONE LOCKING CABLE CLAMP DOES NOT CLEAR THE CONDUIT .5. CLAMPS REPLACED AND CONDUIT ADJUSTED IAW THE MM.Jan 23, 2014 · N932DL · Doug MD88SDR SWAA2014021024960Fairing · crackedWW FAIRING LOWER CHORD CRACKED AT BS 680, RBL 60. R & R CHORD IAW SRM & DRAWING.Jan 22, 2014 · N389SW · Boeing 7373H4SDR DALA14004139512Guide · out of positionDURING INSPECTION, NOTED TAILCONE SLIDE CABLE GUIDE (AFT) ON SLIDE RACK OUT OF POSITION. REPOSITIONED TAILCONE SLIDE CABLE GUIDE (AFT) IAW AMM 25-61-02-400.Jan 17, 2014 · N953AT · Boeing 717200SDR DALA14003640921Hook · wornTAILCONE LT UPPER LATCH HOOK ASSY IS WEARING INTO THE CABLE BLOCK ASSY. INSTALLED NEW LT UPPER LATCH HOOK ASSY AMM AMM 53-53.Jan 15, 2014 · N921DL · Doug MD88SDR DALA14003630921Hook · wornTAILCONE RT UPPER LATCH HOOK ASSY IS WEARING INTO THE CABLE BLOCK ASSY. REPLACED ARM ASSY AND CABLE BLOCK IAW AMM 53-53. OPERATION CHECKED GOOD.Jan 15, 2014 · N921DL · Doug MD88SDR SWIA201436095Structure · crackedCRACK FOUND ON AFT LT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE STRINGER AT FS 909.00 STRINGER 24L. C-CHECK REPAIRED LT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE STRINGER AT FS 909 STRINGER 24L IAW STS EA.Jan 12, 2014 · N708SK · Cndair CL6002C10
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