JASC 5743
Service difficulty reports · 3,097
Reports filed under 5743 · Wing, Landing Gear Attach Fittings, 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 = '5743' 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 = '5743' 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 AALA202207053569Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING RIGHT HAND MAIN LANDING GEAR RETRACTION ACTUATOR FITTING IN THE MAIN LANDING GEAR BAY. REPAIRED FITTING PER SRM 57-26-13-300-008.SDR AALA202206161341Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET BETWEEN RIB 2 AND RIB 3 ON THE REAR SPAR DATUM. REPAIRED BRACKET PER SRM 57-26-13-300-025.SDR N6WA2022061502Panel Support · corrodedCORROSION ON R/H MLG TIRE BURST PANEL. R&R R/H MLG TIRE BURST PANEL IAW CRJ AMM 57-52-32.SDR AALA202205248994Pintle Pin · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR AFT PINTLE PIN WORN. REPLACED PINTLE PIN PER TASK CARD 26T00032001.SDR AALA202205274871Pintle Pin · wornAIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR PINTLE PIN WORN. REPLACED PINTLE PIN PER TASK CARD 26T00032001SDR AALA202205273688Pintle Pin · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR PINTLE PIN WORN. REPLACED PINTLE PIN PER TASK CARD 26T00032001SDR SWIA202265434None · damagedAFT MOUNT BOLT BUSHING DAMAGED ON FLAP FAIRING 523BB (IN HARDWARE BAG). (C-CHECK RO 4/21/2022) REPLACED DAMAGED AFT MOUNT BOLTS AND BUSHINGS ON FLAP FAIRING 523BB ON RACK REF EMB 175 AMM 57-58-23SDR AALA202203315128Trunnion · wornAIRCRAFT WAS GROUNDED: LEFT WING FLAP TRUNNION FITTING HAS WEAR DAMAGE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)SDR FDEA202203270743Slat · gougedLEFT WING #5 SLAT HAS GOUGE IN LOWER SURFACE FROM PROTRUDING RIVET ON FIXED LEADING EDGE. MWT REPAIRED #5 SLAT IAW 767 SRM 57-43-02-2R FIG 201 AND SRM 51-70-10-2R FIG 208.SDR FDEA202203120490Skin · wornLEFT WING #5 SLAT WEDGE LOWER SKIN WORN REPAIRED LEFT WING #5 SLAT WEDGE LOWER SKIN IAW B767 SRM 57-43-02-2R REPAIR 1 FIG. 201 SHEET 1 AND 51-70-10-2R.SDR FDEA202203100457Skin · noneRIGHT WING #9 SLAT TRAILING EDGE WEDGE UPPER SKIN DENTED REPAIRED RIGHT WING #9 SLAT TRAILING EDGE WEDGE UPPER SKIN IAW B767 SRM 57-43-02-2R AND 51-70-10- 2R REPAIR 4SDR AALA202203100393Pintle Pin · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR AFT PINTLE PIN WORN. REPLACED PINTLE PIN PER TASK CARD 26T00032001.SDR AALA202204185470None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT ANCHORAGE FITTING BETWEEN RIGHT WING RIB 2 AND RIB 3 AT THE INNER REAR SPAR. REPAIRED ANCHORAGE FITTING PER SRM 57-26-13-300-025. **SUPPLEMENTAL REPORT FOR AALASDR AALA202204120671None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET (JACK ANCHORAGE FITTING) BETWEEN RIB 2 AND RIB 3. REPAIRED JACK ANCHORAGE FITTING) PER SRM 57-26-13-300-025.SDR AALA202204055470None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT ANCHORAGE FITTING BETWEEN RIGHT WING RIB 2 AND RIB 3 AT THE INNER REAR SPAR. REPAIRED ANCHORAGE FITTING PER SRM 57-26-13-300-025.SDR FDEA202202080245Wedge · gougedRIGHT WING #8 SLAT TRAILING EDGE LOWER SKIN GOUGED AT THE INBOARD AUX TRACK REPAIRED RIGHT WING #8 SLAT TRAILING EDGE LOWER SKIN IAW B767 SRM 57-43-02-2R FIG 201 AND 51-70-10- 2R REPAIR 4.SDR SWIA202264313None · wornLH WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .97MM AT FWD END (C-CHECK RO 2/15/2022) REMOVED AND REPLACED LH INBOARD AFT FLAP TRACK. REF EMB-175 AMM 57-54-25. SEE CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202265008None · scratched* FOUND DEEP SCRATCHES ON THE RH #2 I/B FLAP HINGE ARM ASSY(AREA MARKED) (C-CHECK RO 3/14/2022) BLENDED DAMAGE REF CRJ200 SRM 51-12-00 AND COMPLIED WITH ALL STEPS OF MHI RJ REO 601R-57-54-345 REV-A DATED 2022-03-09. ALL CHECKS GOOD. SEE CONTINUE CARDSDR SWIA202264216None · wornR/H WING OUTBOARD UPPER FLAP TRACK #3 HAS THICKNESS REDUCTION OF 0.0035" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) BLENDED RH OUTBOARD UPPER #3 FLAP TRACK WITH FLAPS EXTENDED. NOMINAL 39MM. REMOVED .16MM MATERIAL REMAINING 3SDR SWIA202264215None · wornR/H WING FLAP TRACK #1A HAS THICKNESS REDUCTION OF 0.010" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) REMOVED AND REPLACED RH WING #1A FLAP TRACK. TW HG4-50097 DUE 6-24-22. REF AMM 57-54-25.SDR SWIA202264214None · wornL/H WING FLAP TRACK #1A HAS THICKNESS REDUCTION OF 0.0095" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) REMOVED AND REPLACED LH WING FLAP TRACK #1A. TW HG4-50097 DUE 6-24-22. REF AMM 57-54-25.SDR 2021FA0000419None · noneL/H AND R/H MLG SIDE BRACE FITTING GOUGE.SDR 2022F00115Brace · gougedTHE LEFT-HAND MAIN LANDING GEAR SIDE BRACE ACTUATOR WAS GOUGED FROM CONTACTING THE ACTUATOR DURING GEAR OPERATION. REPAIR DEEMED MINOR IN SCOPE BY TEXTRON AVIATION ENGINEERING. REPAIR ACCOMPLISHED PER TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ32693M1 DATED DESDR SWIA202163235None · damaged*LEFT WING OUTBOARD FLAP UPPER SKIN €“ 10 SMOKING RIVETS AFT OF THE REAR SPAR ON THE RIB WS254.96. (MARKED) (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW 10EA FASTENERS TO LH WING OUTBD FLAP UPPER SKIN REF REO 670-57-53-303 REV -- DATED 2021-11-21 SDR AALA202111056390Pintle Pin · wornAIRCRAFT IN BASE MAINTENANCE: LEFT MAIN GEAR REAR PINTLE PIN WORN. REPLACED LEFT MAIN GEAR REAR PINTLE PIN PER JOB CARD 26T0003200.SDR KCSA202109281110Support Beam · corrodedL/H MLG SUPPORT BEAM AFT TRUNION BEARING DAMAGED (NOTE: SUPPORT BEAM FOUND TO BE CORRODED IN BEARING BORE)SDR SWIA202162886None · corrodedRH OUTBD FLAP CENTER HINGE ARM UPPER AND LOWER BOLTS AND BUSHING CORRODED (C-CHECK RO 11/28/2021) REPLACED UPPER AND LOWER BUSHINGS OM THE RH OB FLAP CENTER HINGE ARM IAW CRJ 700 AMM 20-31-00-400-802 CONFIG A01, ATTACHED NEW HARDWARE TO HINGE ARM ASSEMBSDR KCSA202109221106Attach Fitting · corrodedLHMLG FWD TRUNION REAR SPAR IB ATTACH FITTING FOR TRUNION HOUSING LOWER BUSHING HAS EVIDENCE OF CORROSIONSDR KCSA202109221105Attach Fitting · corrodedLHMLG FWD TRUNION REAR SPAR IB ATTACH FITTING FOR TRUNION HOUSING UPPER BUSHING HAS EVIDENCE OF CORROSIONSDR SWIA202162884None · corrodedLH OB FLAP CENTER HINGE ARM UPPER AND LOWER BUSHINGS AND ATTACHING HARDWARE IS CORRODED REQUIRES REPLACEMENT (C-CHECK RO 11/28/2021) REPLACED BUSHINGS IAW CRJ 700 AMM 20-31-00-400-802 CONFIG A01, ATTACHED NEW HARDWARE TO HINGE ARM ASSEMBLY SEE CAMP# 234SDR SWAA2021091617116Trunnion · corrodedRIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER O/B LUG OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA NO: 1-A57-3246 REV 12SDR DALA2021091505511Trunnion · corroded(LOG 1945717) DURING INSPECTION FOUND RH MLG OB LOWER BUSHING HOLE AND BUSHING -CORRODED FWD TRUNNION. REPAIRED PER B737 SRM 57-20-90.SDR DALA2021091505510Trunnion · corroded(LOG 1945713) DURING INSPECTION FOUND RMLG FWD TRUNION UPPER OB ATTACH POINT CORROSION. REPAIRED PER B737 SRM 57-20-90.SDR DALA2021091505509Trunnion · corroded(LOG 1945709) DURING INSPECTION FOUND LMLG FWD TRUNION BLOCK LOWER OB ATTACH POINT CORROSION. REPAIRED PER B737 SRM 57-20-90.SDR DALA2021091505508Trunnion · corroded(LOG 1945703) DURING INSPECTION FOUND LMLG FWD TRUNION BLOCK UPPER IB ATTACH POINT CORROSION. REPAIRED PER B737 SRM 57-20-90.SDR DALA2021091505507Trunnion · corroded(LOG 1945696) DURING INSPECTION FOUND LMLG FWD TRUNION BLOCK UPPER OB ATTACH POINT CORROSION. REPAIRED PER B737 SRM 57-20-90.SDR DALA2021091505512Trunnion · corroded(LOG 1945708) DURING INSPECTION FOUND LMLG FWD TRUNION BLOCK LOWER IB ATTACH POINT CORROSION. REPAIRED PER B737 SRM 57-20-90.SDR N6WA2021090801Retainer · crackedANGLE RETAINER IN R/H MLG WHEEL WELL HAS A CRACK.R&R ANGLE RETAINER IN R/H MLG WHEEL WELL IAW CRJ 700 AMM 53-83-85.SDR AALA202109087160Anchor Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING, LEFT HAND MAIN LANDING GEAR ACTUATOR ATTACHMENT ANCHORAGE FITTING BETWEEN WS 700 AND WS 1406, BETWEEN RIB 2 AND RIB 3. REPLACED ANCHORAGE FITTING PER EA 330353.SDR 2021F00273Fitting · chafedREPAIR OF LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE ACTUATOR INBOARD FITTING(S) CHAFE DAMAGE PER TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ31258M1 DATED: 08/27/2021.SDR SWIA202161731None · nicked*LH OUTBOARD FLAP HINGE ARM AT WS 220 €“ NICK ON OUTBOARD FLAP HINGE ARM AT CONNECTION TO HINGE BOX. (C-CHECK RO 10/8/2021) NICK ON LH OUTBOARD FLAP HINGE ARM AT WS 220 €“ ON OUTBOARD FLAP HINGE ARM AT CONNECTION TO HINGE BOX IS BLENDED AND RESTORED SDR SWIA202161730None · gouged*RH INBOARD FLAP GOUGED AT ATTACHMENT TO HINGE BOX (MARKED). (C-CHECK RO 10/8/2021) BLENDED GOUGE ON RH INBOARD FLAP AT ATTACHMENT TO HINGE BOX. RE WORK AREA IS WITHIN LIMITS AND RESTORED TO ORIGINAL REF REO 601R-57-54-337 REV.-- DATED 2021-09-07 . COMPSDR SWIA202162034None · damagedL/H OUTBOARD FLAP #3 O/B HINGE ATTACH POINT DAMAGED (C-CHECK RO 10/29/2021) REPAIRED L/H OUTBOARD FLAP #3 O/B HINGE ATTACH POINT IAW REO 670-57-53-295 REV -- DATED 2021-09-20, TASK CARD 51-900-1002-SKY COMPLIED WITH.SDR A6WA202108247939None · dentedRIGHT HAND WING LEADING EDGE SKIN (DWG: 601R12057, REF) HAS A DENT BETWEEN WS149.580 Ï¿½ WS158.523. PERFORMED DRESS BACK OF DENT ON RIGHT HAND WING LEADING EDGE SKIN (DWG: 601R12057 REF) BETWEEN WS149.580 Ï¿½ WS158.523. DENT DIMENSIONS L = 5.750Ï¿½ X W = 1SDR SWIA202161709None · gouged* R/H INBOARD FLAP, INBOARD AFT FLAP BOX ATTACH FITTING, 2 EA. CENTER AFT ATTACH LUGS ARE GOUGED ON THEIR AFT SIDES, MARKED. (C-CHECK RO 10/8/2021) REMOVED CHAFE FROM R/H INBOARD FLAP, INBOARD AFT FLAP BOX ATTACH FITTING, 2 EA. CENTER AFT ATTACH LUGS. SDR SWIA202161983None · gougedINBD FLAP INBD HINGE BOX ATTACHMENT FITTING AFT INBD LUG HAS GOUGE (C-CHECK RO 10/29/2021) COMPLIED WITH ALL STEPS OF MHIRJ REO 670-57-21-921 REV -- DATED 2021-09-03 FOR INBD FLAP INBD HINGE BOX ATTACHMENT FITTING AFT INBD LUG. COMPLIED WITH SKYWEST TASSDR SWIA202161550None · chafed*LH OUTBOARD FLAP CENTER HINGE ARM €“ INBOARD GUIDE PLATE CHAFED. (C-CHECK RO 10/4/2021) REPAIR CHAFED DAMAGE ON LH OUTBOARD FLAP CENTER HINGE ARM €“ INBOARD GUIDE PLATE REF REO 601R-57-54-336 REV -- DATED 2021-08-28 .ORIGINAL THICKNESS .050" , REMAIISDR DALA2021080604504Trunnion · corroded(LOG 1899695) DURING INSPECTION FOUND LEFT MLG FWD TRUNNION FITTING (ON AIRCRAFT) O/B LOWER BUSHING IS MIGRATED AND HAS PITTING AT THROUGH BORE. CORROSION REPAIRED PER B737 SRM 57-20-90.SDR DALA2021080604503Trunnion · corroded(LOG 1899694) DURING INSPECTION FOUND LEFT MLG FWD TRUNNION FITTING (ON AIRCRAFT) O/B UPPER BUSHING HAS PITTING AT THROUGH BORE. CORROSION REPAIRED PER B737 SRM 57-20-90.SDR DALA2021080604502Trunnion · corroded(LOG 1899693) DURING INSPECTION FOUND LEFT MLG FWD TRUNNION FITTING (ON AIRCRAFT) I/B LOWER BUSHING HAS PITTING AT THROUGH BORE AND ON I/B FACE. CORROSION REPAIRED PER B737 SRM 57-20-90.
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