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 CALA2017041701018Skin · damagedRIGHT FWD WING TO BODY FAIRING UPPER LEADING EDGE AREA HAS SCRIBE LINES. ACCOMPLISHED INTERIM REPAIR AT FUSELAGE BETWEEN STA 500A AND 500D AND BETWEEN STR 16R AND STR 21R IAW EC/RA 5330-06041.SDR DALA2017041703102Cable · frayedTAILCONE CABLE FRAYED. REPLACED THE CABLE IAW AMM 53-53-00.SDR SWIA201743278Tail Cone · damagedDAMAGE FOUND ON THE TAIL CONE. REPLACED THE TAILCONE IAW AMM.SDR DALA2017041403012Pin · wornFOUND PIN FOR TAILCONE RELEASE IN AFT ACCESSORY COMPARTMENT WORN. REMOVED AND REPLACED THE PIN IAW AMM 53-53-00.SDR SWAA2022012036924Fairing · delaminatedINTERNAL DELAMINATION ACCESS PANEL #193D ON WING TO BODY FAIRING ON LOWER FUSELAGE / REPAIRED ACCESS PANEL #193D ON WING TO BODY FAIRING LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2SDR SWAA2022012078120Fairing · delaminatedDELAMINATED INNER SKIN OF ACCESS PANEL 194CL ON LOWER FUSELAGE / REPAIRED ACCESS PANEL 194CL ON LOWER FUSELAGE IAW B737-300 SRM 51-70-04-2R-3 REP 3SDR IPXA2017042816590Skin · wornINSPECTION TYPE: 3C, TAIL CONE REPAIR DOUBLER HAS WEAR AT BS 2156.6, RBL 36.5, Z=40 AND 60.1. REPAIRED THE TAIL CONE IAW EA 011-5320-01-A6753, REV I/R, AND EO MD11-5350-64001-A.SDR DALA2017041102926Cable · frayedTAILCONE CABLE FRAYED. REPLACED TAILCONE CABLE IAW AMM 20-10-01.SDR DALA2017041102901Rivet · looseTAILCONE UPPER LEFT LOCK BRACKET PULLING LOOSE FROM TAIL CONE. REMOVED LOOSE RIVETS AND INSTALLED NEW RIVETS PER MD88 SRM51-30-2.SDR EBVR20170410001Skin · crackedFOUND CRACKS IN TWO RIBS, INSIDE STINGER. FOUND DURING APU EXHAUST DETAILED INSPECTION. REPAIRED THE AREAS ON TWO FRAMES OF THE APU STINGER IAW AQRD ERO-890917 REV IR. MAJOR REPAIR.SDR SWAA2022011978078Fairing · delaminatedDELAMINATED ACCESS PANEL 194 CL ON LOWER FUSELAGE / REPAIRED ACCESS PANEL 194CL ON LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REP 2SDR SWAA2022011881538Access Panel · crackedCRACK ACCESS PANEL # 193 AR LOWER AREA ON BODY STATION 540 ON LOWER FUSELAGE / REPAIRED ACCESS PANEL #193AR LOWER AREA ON BODY STATION 540 ON LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REP.2 PAR 4SDR SWAA2022011981539Access Panel · crackedCRACK UPPER AREA ACCESS PANEL # 193AR ON BODY STATION 540 ON LOWER FUSELAGE / REPAIRED UPPER AREA ACCESS PANEL #193AR ON BODY STATION 540 ON LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-3 PAR 4SDR SWAA2022011711256Panel · delaminatedL/H FWD W/W CUTOUT PANEL 193AL HAS LEADING A 12' LEADING EDGE DELAMINATION SEVERAL PLYS DEEP. MOD / REPAIRED PANEL 193A1 PER SRM 53-40-70-2R-1SDR AALA201704129030Splice Plate · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON WING TO BODY FAIRING SPLICE PLATE AT STATION 800 AND BL-0. REPLACED SPLICE PLATE PER SRM 51-40-02.SDR DALA2017041002924Release Mech · out of adjustTAIL CONE FAILED INTERNAL RELEASE MECHANISM TEST. ADJUSTED TAIL CONE JETTISON. PULL WAS WITHIN LIMITS.SDR IPXA2017042416425Doubler · wornINSPECTION TYPE: 3C, TAIL CONE AT BS 2165 LT INTERNAL DOUBLER HAS DEEP WEAR. REPAIRED THE TAIL CONE INTERNAL DOUBLER IAW EA 011-5350-01-A6743, REV I/R, AND EO MD11-5350-63879-A.SDR IPXA2017042316387Fitting · wornINSPECTION TYPE: 3C, EXTENDED TAILCONE SNUBBER ATTACH FITTING WORN. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SNUBBER FITTING IAW EA 011-5320-01-A6761, REV IR, AND EO MD11-5350-64004-A.SDR IPXA2017041416137Doubler · chafedINSPECTION TYPE: 3C, FORWARD EXTENDED TAILCONE INTERNAL DOUBLER CHAFED BS 2165, RBL 36.5, Z 41 - 60.1. REPAIRED THE DAMAGE IAW EA 011-5350-01-A6741, REV IR, AND EO MD11-5350-63878-A.SDR IPXA2017041416133Radome · erodedINSPECTION TYPE: 3C, RADOME EXTERIOR SKIN ERODED. REMOVED AND REPLACED THE RADOME IAW AMM 53-51-01.SDR SWAA2022011427107Fairing · elongated5 FASTNERS HOLES ARE ELONGATED ON #3 FAIRING (542BB) AFT I/B SIDE SEAL (MARKED) / REPAIRED PER SRM 57-53-70-2R-2 AND 51-70-04-2R-9.SDR SWAA2022011417471Panel · delaminatedPANEL 193CL HAS A DELAMINATION ON THE INNER SURFACE; 8' FROM THE I/B EDGE; 6' FROM THE AFT EDGE / PANEL 193CL WITH A DELAMINATION ON THE INNER SURFACE 8' FROM THE I/B EDGE; 6' FROM THE AFT EDGE WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR REXA2017033000431Channel · crackedAFT WING TO BODY FAIRING SPLICE CHANNEL IS CRACKED. REMOVED CRACKED CHANNEL ON AFT WING TO BODY FAIRING, AND REPLACED W/NEW SERV CHANNEL IAW SRM 51-42-13.SDR SWAA2022011446613Seal · crackedLEFT UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED L/H UPPER SLIDING SEAL PER AMM 53-31-31. OPS CHECK TO BE PERFORMED ON ACO #8453-53.SDR SIMA20170326002Rib · crackedSHEET METAL UNDER NR 2 WING LOOKS CRACKED BY WHEEL WELL. INSPECTED A/C AND FOUND 5.5" CRACK ON RT MLG AFT RIB PN 145-72166-002 ITEM TRANSFERRED TO LOG PAGE 4069199 ITEM 1. C/W PERMANENT REPAIR ON RT MLG AFT RIB IAW ERS-EM-5300-2647.SDR DALA2017032602422Pin · wornTAIL CONE LOCK PINS WORN, RIGHT SIDE UPPER & LOWER. R & R BOTH RT UPPER & LOWER LOCK PIN ASSEMBLIES IAW AMM 53-53-00-501.SDR DALA2017032802472Guide · wornBAD VIBRATION AT FRONT OF AIRPLANE CLIMBING OUT ABOVE 300 KNOTS. PERFORMED GVI FOUND EXCESSIVE PLAY ON RADOME GUIDE PIN HOLES R&R RADOME REF AMM 53-51.SDR DALA2017032102262Cam · wornFOUND BASE OF THE TAILCONE RELEASE MECHANISM CAM WORN. REPLACED TAILCONE RELEASE MECHANISM CAM BASE IAW AMM 53-53-02.SDR DALA2017032102261Skin · crackedLOWER AFT TAIL CONE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED TAILCONE IAW CARD 5350-0177-0101.SDR R61A201703110234Rib · crackedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED A CRACK ON THE MID FAIRING AFT HANGING SUPPORT RIB AT THE UPPER RT SIDE. MAINTENANCE REMOVED, FABRICATED AND INSTALLED DOUBLER REPAIR AT MID FAIRING AFT HANGING SUPPORT RIB IAW ETD 2017-170-024147.SDR DALA2017031302037Valve · failedTAILCONE DISPLACEMENT BOTTLE VALVE BALL ASSEMBLY WON`T ENGAGE IN THE LOCK POSITION WITH OR WITHOUT CABLE INSIDE HOUSING. REMOVED AND REPLACED.SDR SWAA2017032112585Skin · delaminatedTAIL CONE SKIN DELAMINATED AT BS1156 +27", LBL 12. REPAIRED SKIN IAW SRM.SDR REXA2017030900370Support Channel · crackedAFT WING TO BODY FAIRING SUPPORT CHANNEL IS CRACKED. REMOVED AND REPLACED THE SUPPORT CHANNEL IAW SRM-51-42-13.SDR SWAA2017032112629Skin · delaminatedRIGHT TAILCONE SKIN DELAMINATED AT BS 1156 +6.5. REPAIRED THE SKIN IAW SRM.SDR DALA2017030801876Support Fitting · wornTAIL CONE CAM MECHANISM SUPPORT FITTING WORN, AND FAILED TORQUE CHECK. REMOVED THE TAIL CONE SUPPORT FITTING AND REPLACED THE SHAFT AND SUPPORT FITTING IAW AMM 53-53-02 AND AMDS 5350-010770101.SDR DALA2017030601775Bracket · crackedTAIL CONE RIGHT UPPER BAYONET FITTING BRACKETS CRACKED. DRILLED REPLACEMENT BRACKETS. TREATED, PRIMED & PAINTED PART. INSTALLED THE BRACKETS IAW SRM 51-30-02.SDR DALA2017030501771Cam · no testTAILCONE RELEASE MECHANISM CAM TORQUE CHECK FAILED. REPLACED THE RELEASE MECHANISM CAM SUPPORT BRACKET IAW AMM 53-53-02.SDR DALA2017030201713Release Cable · brokenAFT ACCESSORIES COMPARTMENT: BROKEN RELEASE TAILCONE CONTROL CABLE WIRES AT 10 HRS POSITION. RELEASE TAILCONE CONTROL CABLE AT 10 HRS POSITION WAS REPLACED AND ADJUSTED PER AMM 20-10-17-201 AND PER AMM 53-53-00-501.SDR DALA2017030101645Pin · out of adjustTAILCONE RELEASE MECHANISM CAM ASSY. PIN IS IMPROPERLY INDEXED ON SPLINE. REINDEXED CAM RELEASE PIN PER MD88 AMM 53-53-02-201, O.K. FOR SERVICE.SDR DALA2017022801612Cable · frayedTAILCONE CABLE FRAYED. REPLACED THE CABLE IAW AMM 53-53-00.SDR DALA2017022301494Cam · wornTAILCONE CAM RELEASE MECHANISM HAS END PLAY. REMOVED AND REPLACED TAHE CAM IAW AMM 53-53-02.SDR DALA2017022401543Receptacle · wornTAILCONE HAS SEVERAL GUIDE PIN RECEPTACLES WORN OUT OF ROUND. REMOVED AND REPLACED IAW SRM 51-41-01.SDR DALA2017022101437Former · corrodedLT FILLET FORMER AT STA 851 HAS CORROSION AROUND SCREW HOLES AT LOWER END. REPLACED LT FILLET FORMER "ITEM-10 ANGLE" AT STA 851 THAT WAS CORRODED BEYOND LIMITS NOMINAL .050" LOSS=.023 REMAINING .027" IAW SRM 51-41-02 0G, 53-20-71 0I-1 AND DWG 5971058.SDR DALA2017030301743Cable · misroutedTAIL INTERIOR EXTERNAL RELEASE LOCKING HANDLE CABLE MISROUTED. CORRECTED IAW AMM.SDR UIEA2017021600189Support · corrodedSUPPORT FWD FUSELAGE LT LOWER WING TO BODY FAIRING AT STA 960 - 980 LBL 3 - 4. REMOVE DAMAGED PART IAW SRM 51-40-02-0G-0 REV 18. INSTALL NEW PART P/N 65B06976-5 IAW SRM 51-40-02-0G-0 REV 78 AND DWG NR 65B06976 SH2 REV G. JOB COMPLETED AND CONDITION CHECK NORMASDR UIEA2017021600190Angle · corrodedANGLE, FWD FUSELAGE LOWER WING BODY FAIRING AT STA 920 RBL 3 - LBL 3. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 78. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 78 AND DWG 142U0130 SH1 REV A AND DWG 65N06704 SH2 REV F. JOB COMPLETED AND CONDITION CHECK SDR SCNA20170201036Fairing · damagedLOWER FUSELAGE WING TO BODY PANEL 192AL HAS EXPOSED COMPOSITE. CLEANED, PREPPED, RESIN SWEPT, AND RESTORED EXTERIOR FINISH TO LWR FUSELAGE WING TO BODY PANEL.SDR SCNA20170201010Fairing · delaminatedWHEN REMOVING RT WING TO BODY FAIRING 195CR, FOUND AFT BOTTOM EDGE AT RADIUS DELAMINATED. REPAIRED THE FAIRING.SDR SCNA20170201009Fairing · puncturedWING TO BODY FAIRING PANEL 194CL IS PUNCTURED ON OUTER FACE. REPAIRED THE FAIRING.SDR IPXA2017030114591Beam · gougedINSPECTION TYPE: 3C, FWD EXTENDED TAIL CONE AT BS 2165, BEAM HAS GOUGE DAMAGE. REPAIRED THE TAIL CONE BEAM IAW EA 011-5320-01-A6615 REV I/R, AND EO MD11-5350-63293-A.
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