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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR QXEA2012012300015Structure · damagedEIGHT SMOKING RIVETS, LOCATED ON LT FWD WING TO FUSELAGE FAIRING. RIVETS ARE LOCATED AT APPROX STA 310 AND PORT STR 6. R & R RIVETS IAW SRM 51-42-45-02-01. PAINTED RIVETS IAW SRM 51-25-05-02-01.SDR DALA1202530964Release System · wornAIRCRAFT FAILED THE TAIL CONE FUNCTIONAL TEST ON 3 SEPARATE WORK CARDS. THE CONE FAILED TO DROP WHEN THE BAYONET SLIPPED PAST THE TRIGGER ARM ASSEMBLY. MAINTENANCE VERIFIED THAT THE BAYONET WAS ENGAGED CORRECTLY BUT AS IT WAS PULLED FORWARD THE TRIGGER PULLSDR SWIA201229300Fairing · delaminatedCENTER AFT WING TO FUSELAGE FAIRING HAS DELAMINATION ON LEFT UPPER FORWARD SIDE. (SERVICE) REPAIRED DAMAGE DELAMINATION.SDR SWIA201229296Fairing · delaminatedLEFT MID SECTION WING TO FUSELAGE FAIRING HAS DELAMINATION ON LOWER AFT SECTION. (SERVICE) REPAIR DELAMINATION.SDR DALA1201340998Release System · failedTHE TAIL CONE RELEASE FUNCTIONAL TEST FAILED OPN 6908. THE PULL TEST SCALE READ 30 LBS, WHICH EXCEEDS ALLOWABLE LIMITS. (NO CORRECTIVE ACTION IDENTIFIED. TO144 2012-D0038)SDR UIEA2012010900006Fairing · damagedLT WING TO BODY FAIRING PANEL DAMAGE AT BS 1550. ACCOMPLISHED PART 1 OF EO 4453A671.SDR FDEA201201070042Fairing · corrodedRT WING TB FAIRING 192AR CORRODED CIRCUMFERENCE OF PANEL AT FASTENER HOLES. CHECKED LIMITS OF ALL REWORKED AREAS. FOUND IN LIMITS EXCEPT 1 EA SPOT AT RBL 2.75 ORIGINAL THICKNESS .075 REMAINING THICKNESS .042 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II, LSDR SWIA201229115Bushing · vibrationLOW FREQUENCY VIBRATION THAT COULD BE FELT THROUGH THE AIRFRAME WHILE CLIMBING. (FLT 5327) REPLACED BELLY FAIRING FITTING BUSHINGS.SDR DALA1200380992Spring · missingTHE TAIL CONE FAILED TO UNLOCK AND DROP DURING THE FUNCTIONAL CHECK OPN 6908. MAINTENANCE FOUND THE SPRING IN THE T-PIN PLUNGER WAS MISSING SO THEY INSTALLED A NEW SPRING, CLEANED, AND LUBRICATED THE CLIPS AT THE T-PIN PLUNGER. SYSTEM REQUIRES AN OPERATIONALSDR NSVA2011385Tail Cone · misrepairedDOUBLER REPAIR TO UPPER LT TAIL CONE SKIN AT STA 793 IS NOT IN DAMAGE LOG OR ON FILE. THE RIVET PATTERN AROUND THE CUTOUT IS IRREGULAR AND DOES NOT HAVE A DOUBLE ROW AT BOTTOM EDGE OF CUTOUT. THE FORWARD EDGE OF THIS REPAIR IS AT THE SKIN SPLICE OF FRAME STASDR NSVA2011383Tail Cone · misrepairedFOUND DOUBLER REPAIR TO RT UPPER TAIL CONE ABOVE AFT HORIZONTAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. RIVET SPACING AND CUTOUT DOES NOT CONFORM TO THE PRINCIPLES OF SRM 53-90-10-202. REFER TO SAAB STATEMENT SDS023483 DATED 12-20-11, TD 340-53-11-101 & MSDR NSVA2011382Tail Cone · misrepairedDOUBLER/TRIPLER REPAIR TO RT UPPER TAIL CONE JUST BELOW VERTICAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS MISSING MULTIPLE RIVETS IN THE FIELD. THERE IS A DENT IN THE AFT LOWER AREA OF THE PATCH AT STA 823. THE RIVET PATTERN AROUND THE CUTOSDR NSVA2011378Tail Cone · misrepairedDOUBLER/TRIPLER REPAIR TO RT UPPER TAIL CONE JUST BELOW VERTICAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS MISSING MULTIPLE RIVETS IN THE FIELD. THERE IS A DENT IN THE AFT LOWER AREA OF THE PATCH AT STA 823. THE RIVET PATTERN AROUND THE CUTOSDR CA120103008Fairing · dislodged(CAN) UPON REACHING CRUISE ALTITUDE OF FL 240 EXPERIENCED PRONOUNCED BUFFETING OF AIRFRAME AT APPROXIMATELY 300 KTS. BUFFETING SUBSIDED BY 250 KTS. TRIED DIFFERENT ALTITUDES, BUT EXPERIENCED SAME EFFECT TIME AFTER TIME. NO WARNING OR CAUTION MESSAGES. ENGINE SDR UIEA2011122100725Fairing · damagedDURING WALKAROUND, DAMAGE WAS FOUND TO THE RT AFT WING TO BODY FAIRING AT BS 1560, APPROX STRINGER 38R.; THE AIRPLANE HAS 8,082 TFC AND 60,711 TFH AT THE TIME OF THE PART 1 REPAIR. THE DAMAGE CONSISTS OF A HOLE IN THE WING TO BODY FAIRING HONEYCOMB STRUCTURE MSDR MU1Z2011020200007Radome · damagedDURING DESCENT STRONG HIT WAS FELT IN THE RADOME ZONE, WITH VISUAL CONFIRMATION OF BIRD STRIKE AFTER PARKING (RADOME BROKEN) THE MEASURES OF THE DAMAGE ARE THE FOLLOWING: LENGTH: 190 MM, WIDE: 130 MM, DEPTH: 5 MM. DENT DAMAGE (BIRD STRIKE) IN THE BULKHEAD ARSDR CWQR2011120530Drag Angle · crackedDURING SCHEDULED MX THE WING TO FUSELAGE FAIRINGS WERE REMOVED. FOUND 3 LOCK FASTNERS FROM THE WING SKIN TO DRAG ANGLE, WITH CRACKS IN THE DRAG ANGLE BRACKET. THE CRACKS ON THE DRAG ANGLE WERE HORIZ FROM EACH LOCK FASTERNER AND MOVING TOWARDS THE ADJACENT FASDR CWQR2011120529Drag Angle · crackedDURING SCHEDULED MX, FOUND 3 LOCK FASTENERS FROM THE WING SKIN TO DRAG ANGLE, WITH CRACKS IN THE DRAG ANGLE BRACKET. THE CRACKS ON THE DRAG ANGLE WERE HORIZONTAL FROM EACH LOCK FASTENER AND MOVING TOWARDS THE ADJACENT FASTNERS.SDR IXXA110078OFairing · contaminatedDURING TAKEOFF, THE CREW SMELLED A STRONG FUEL ODOR, THE PACKS WERE TURNED ON AND FUEL ODOR WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX CLEANED RESIDUAL FUEL FROM RT WING TO BODY FAIRING IAW AMM 20-30-83/201. ACFT WAS RETURNED TO SERVICE.SDR DALA1200720929Mechanism · failedDURING TAIL CONE RELEASE, THE CAM TORQUE CHECK TEST FAILED. TAIL CONE RELEASE MECHANISM WAS REPLACED PER MD-88 AMM 53-53-02. 2ND OPERATIONAL CHECK PASSED PER MD88 AMM 53-53-02.SDR A6WA201240030Fairing · chafedLOWER FUSELAGE UNDER EACH OTBD ENDS OF MLG FWD FAIRING HAVE CHAFING DAMAGE. REPAIRED DAMAGE IAW REO 601R-57-21-880.SDR VNAA2011112300015Radome · damagedAT CAK, CREW REPORTED BIRD STRIKE TO RIGHT SIDE OF NOSE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, REMOVED AND REPLACED RADOME AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.SDR AALA20111116AFW03Tail Cone · dentedDENT AT TAIL CONE LEFT SIDE AT BASE OF RUDDER. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01-2R-14.SDR IPXA11570591Ring · corrodedINSPECTION TYPE:C-CK, AFT TAIL CONE RING HAS CORROSION. FABRICATED NEW TAIL CONE AFT RING IAW DWG 148N1606.SDR UALA2011111006150Seal · faultyCREW REPORT: F/A REPORTS VIBRATION AND HUMMING NOISE IN FRONT OF COACH CABIN BACK TO WINDOW EXITS. ACCOMPLISH VISUAL INSPECTION FOR OBVIOUS DAMAGE AND DEFECTS. FOR POSSIBLE OVERWING FAIRING SEALS. PANEL 192BT WAS FOUND TO HAVE A SMALL PIECE OF RUBBER SEAL SDR UALA2011110706070Radome · damagedAT GEAR RETRACTION, AFTER TAKEOFF, CREW HEARD A LOUD BANG FROM NOSE GEAR AREA. PLEASE INSPECT NOSE GEAR, WHEEL WELL & IMMEDIATE AREA FOR ANY DEFECTS OR ABNORMALITIES. REPORT FINDINGS TO SAMC. SAMC TEXT: RADOME DAMAGED, PART MOVING IN. REPLACED RADOME.SDR A6WA201141104Fairing · chafedFUSELAGE FAIRING CHAFING AT INBD WING ROOT BEHIND STUB FAIRING ON LT SIDE. REPAIRED IAW REO 601R-53-41-610.SDR UALA2011102105688Radome · dentedDENT ON RADOME MEASURES APPROX 18 IN W BY 20 IN HIGH WITH SOFT-SPONGY AREAS. BEYOND LIMITS.SDR C2XA11TY161Radome · damagedLIGHTNING STRIKE ON NOSE WITH BURNS AND RADOME COATING DAMAGE. UPON LIGHTNING STRIKE INSPECTION FOUND SEVERAL AREAS OF DAMAGE. REPAIRED LT AILERON, LT WING TIP, REPLACED LWR TDR ANTENNA, REPLACED VHF 2 ANTENNA, REPLACED DME 2 ANTENNA, REPLACED RADOME, REPAIRSDR USAA2011101800055Fairing · cracked2S CHECK - ON LEFT WHEEL WELL FAIRING AT FLAP CARRIAGE FR53.2, BETWEEN S32L TO S37L. REPAIRED FAIRING AT FLAP CARRIAGE FR53.2, BETWEEN S32L TO S37L IAW A330 SRM 53-35-14.SDR COEA2011101309919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRING REMOVABLE INTERCOSTAL AND ATTACH ANGLES AT OUTBOARD EDGE OF PANEL 192FR, FR 23A-24A ARE CORRODED. (LENGTH 8", WIDTH 2", DEPTH .024"). REMOVED AND REPLACED INTERCOSTAL CHANNEL WITH OEM PART.SDR COEA2011101308919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRING REMOVABLE INTERCOSTAL AND ATTACH ANGLES OUTBOARD EDGE OF PANEL 192FR, FR 22A-23A ARE CORRODED. (LENGHT 6", WIDTH 1.5", DEPTH .024") REMOVED AND REPLACED INTERCOSTAL CHANNEL WITH OEM PART.SDR COEA2011101307919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRING REMOVABLE INTERCOSTAL AND ATTACH ANGLES AT OUTBOARD EDGE OF PANEL 191FL, FR 23A-24A ARE CORRODED. (LENGTH 5", WIDTH 3", DEPTH .071") REMOVED AND REPLACED CHANNEL WITH OEM PART.SDR COEA2011101306919Intercostal · corrodedHEAVY CK COE / LEVEL 2 CORROSION: BELLY FAIRINIG REMOVABLE INTERCOSTAL AND ATTACH ANGLES AT OUTBOARD EDGE OF PANEL 191FL, FR 22A-23A ARE CORRODED. (LENGTH 8", WIDTH 2", DEPTH .028") REMOVED AND REPLACED INTERCOSTAL CHANNEL WITH OEM PART.SDR DALA1157220968Tail Cone · no testWHILE PERFORMING THE TAIL CONE RELEASE FUNCTIONAL CHECK OPN 6908AD THE TAIL CONE WOULD NOT DEPLOY. NON-ROUTINE CARDS WERE WRITTEN FOR THE REQUIRED REPAIRS.SDR IPXA1569517Support Angle · wornINSPECTION TYPE:C1, RT WING, WING TO BODY SUPPORT STRUCTURE IS WORN AT STA 1147 AT MOST INBD T/E PANEL SUPPORT ANGLE. R & R CHORD IAW SRM 51-40-02; SRM 51-40-05; SRM 53-40-71-0I1 SRM 53-00-71-1A1.SDR HALA2011092600439Splice · damagedRT FUSE AFT BODY WING BODY SPLICE-SCREW DAMAGE ON OTBD SIDE - DEPTH .010", DIAMETER .150" LOCATED - RBL 97.42, REAR SPAR WING/BODY AFT LOWER SPLICE PLATE. AREA REWORKED PREVIOUSLY. INSTALLED CORRECT LENGTH SCREWS. REWORK OF DAMAGED AREA CARRIED OUT IAW ANZ TSDR DALA1155000940Lock Pin · lack of lubeDURING TAIL CONE FUNCTIONAL CHECK RELEASE SYSTEM, BULKHEAD DOOR CONTROL ARM FAILED TO DEPLOY. MAINTENANCE REMOVED AIRSTAIR FORWARD CEILING PANELS AND DOOR FRAME COVERS FOR ACCESS. LOCK PINS WERE LUBRICATED PER AMM 53-53. PERFORMED OPN 6908AD. OPERATION TESSDR UALA2011092105112Fairing · damagedKEEL BEAM FAIRING 149BL HAS DAMAGE.SDR UALA2011091905041Tail Cone · damagedAPU TAIL CONE COMPARTMENT DAMAGED FROM WING TIP CONTACT OF AIRCRAFT 6664. TAGGED COCKPIT, DISCONNECTED ELEC SYS COMPONENTS & APU BLEED DUCT SECTION IN PREPARATION FOR TAIL CONE REPLACEMENT. REPLACED TAIL CONE.SDR A6WA201140922Seal · chafedLT SIDE OF FUSELAGE IS CHAFED BY THE LT INBD SEAL OF THE WING AND THE LT STUB FAIRING COMPLIED WITH REO 601R-53-41-341.SDR DALA1152006309Fitting · corrodedCORROSION WAS FOUND ON BODY FAIRING CLIP STA 880 BL 0. S: 1"X0.8". REPLACED WITH NEW CLIP .SDR DALA1151636309Support · crackedRADOME SUPPORT CRACK BS 134 RBL6 L=0.8". REPLACED THE SUPPORT WITH NEW ONE PER B747-400 SRM 51-40-02 P1.SDR DALA1151966309Fitting · corrodedCORROSION WAS FOUND ON TWO BODY FAIRING CLIPS STA 920. BL 0. S: 1"X0.8" REPLACE THE CLIPS WITH THE NEW ONE PER B747-400 SRM 51-40-02.SDR VNAA2011090800002Radome · damagedCREW REPORTED A LIGHTNING STRIKE IN FLIGHT EN ROUTE FROM CAK TO PHL. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED RADOME, TAT PROBE, ATC ANTENNA AND STATIC WICKS. DAMAGE (BURN MARKS) WAS REPAIRED ON LEFT ASDR DALA1151586309Support · corrodedCORROSION WAS FOUND ON BODY FAIRING SUPPORT STA 987 LBL 50.S:1"X0.8". MAINTENANCE REPAIRED SUPPORT FLANGE.SDR DALA1151606309Fairing · corrodedSEVERAL CORROSION WERE FOUND ON BODY FAIRING 880. BL 0-LBL 50. S: 0.9"X0.9". MAINTENANCE REPAIRED FAIRING SUPPORT FLANGE.SDR DALA1151596309Support · corrodedSEVERAL CORROSION WERE FOUND ON BODY FAIRING SUPPORT STA 880 BL 0-RBL 40. S: 0.9"X0.9". MAINTENANCE REPAIRED FAIRING SUPPORT FLANGE.SDR DALA1150896309Support · corroded8/190 SEVERAL CORROSION WERE FOUND ON BODY FAIRING SUPPORT STA 1660. LBL 40-60. S=0.8"X0.8" LOG PAGE ENTERED AND DEFERRED FOR SDR REPORTING. MAINTENANCE PERFORM REPAIRED PER ER/A 495578-14 REV ORIGINAL. RII COMPLETED.SDR DALA1150906309Support · corroded5/190 A CORROSION WAS FOUND ON SUPPORT OF BODY FAIRING STA 9875 LBL 20. S:1"X5" LOG PAGE ENTERED AND DEFERRED FOR SDR REPORTING. MAINTENANCE REPAIR 3 FIG 201 REPAIRED THE SUPPORT FLANGE.
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