JASC 5744

Service difficulty reports · 2,730

Reports filed under 5744 · Wing, Control Surface 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 = '5744'
  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 AALA20151015006Support Fitting · crackedRIGHT WING, GND SPOILER ACTUATOR SUPPORT FITTING CRACKED AT FWD INBD CHAMFER. REPLACED RT WING GND SPOILER SUPPORT FITTING WITH NEW FITTING.Oct 14, 2015 · N984TW · Doug DC983SDR DALA2015101506157Attach Bracket · crackedRIGHT WING AILERON INBD ACTUATOR ATTACH BRACKET OTBD LUG IS CRACKED, MEASURED AT .610". REPLACED RT WING INBD AILERON ACTUATOR ATTACH BRACKET IAW SRM 51-42-11.Oct 14, 2015 · N344NB · Airbus A319114SDR FDEA201510023043Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE SURFACE CORRODED. REPAIRED IAW EA 1-5750-T0320588 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 2, 2015 · N624FE · Doug MD11FSDR FDEA201510023042Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE BORE CORRODED. A REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0320588 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 2, 2015 · N624FE · Doug MD11FSDR FDEA201510023041Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.Oct 2, 2015 · N624FE · Doug MD11FSDR FDEA201510023040Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION.Oct 2, 2015 · N624FE · Doug MD11FSDR FDEA201510013028Hinge · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11FSDR FDEA201510013027Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11FSDR FDEA201510013026Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11FSDR FDEA201510013025Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11FSDR FDEA201510013024Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, BARREL NUT HOLE BORE CORROSION.Oct 1, 2015 · N624FE · Doug MD11FSDR FDEA201509303002Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE CORROSION.Sep 30, 2015 · N624FE · Doug MD11FSDR FDEA201509303001Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION.Sep 30, 2015 · N624FE · Doug MD11FSDR FDEA201509303000Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION.Sep 30, 2015 · N624FE · Doug MD11FSDR FDEA201509302999Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION.Sep 30, 2015 · N624FE · Doug MD11FSDR FDEA201509292994Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. A REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0320592 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292993Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. REPAIR BUSHING FABRICATED& INSTALLED IAW EA 1-5750-T0320592 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292986Hinge · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0320513 PART 1 STEP 1C. REFER TO WRI 57502481 FOR WORK DETASep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292985Hinge · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0320513 PART 1 STEP 1C. REFER TO WRI 57502481 FOR WORK DETASep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292983Hinge · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0320513 PART 1 STEP 1 & SHOULDER BUSHING FABRICATED BY MACHINING & INSTSep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292982Hinge · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0320513 PART 1 STEP 1 & SHOULDER BUSHING FABRICATED BY MACHINING & INSTSep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292981Hinge · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0320513 PART 1 STEP 1B. REFER TO WRI 57502481 FOR WORK DETAILS. REPSep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292980Hinge · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0320513 PART 1 STEP 1D. REFER TO WRI 57502481 FOR WORK DETAISep 29, 2015 · N624FE · Doug MD11FSDR FDEA201509292979Hinge · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0320513 PART 1 STEP 1D. REFER TO WRI 57502481 FOR WORK DETAISep 29, 2015 · N624FE · Doug MD11FSDR AALA20150922021Hinge · corrodedLEFT WING AILERON HINGE NR 3 RIB SURFACE FOUND CORROSION. REPAIRED LT WING AILERON HINGE NR 3 RIB SURFACE AREA IAW SRM 57-51-02-2R-3 REPAIR 3.Sep 23, 2015 · N795AN · Boeing 777223SDR ABXA20150914185Support Fitting · corrodedFLAP SUPPORT NR 1, TENSION BOLT HOLE NR 1 HAS A DEFECT INDICATION, REFERENCE JC EA5750006-001. REAMED HOLE TO .672, NO FURTHER DEFECTS NOTED, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-43, PART NAME, FLAP SUPPORT FITTING NR 1, Sep 14, 2015 · N315AA · Boeing 767223SDR ABXA20150914184Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 3 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED FASTENER HOLE TO .8285, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2,Sep 14, 2015 · N315AA · Boeing 767223SDR ABXA20150914183Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED HOLE TO .829, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2, WS LOCATISep 14, 2015 · N315AA · Boeing 767223SDR ABXA20150914182Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 1 HAS DEFECT INDICATION, REFERENCE JC EA57500018-001. REAMED FASTENER HOLE TO .8285, NO FURTHER DEFECTS, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR Sep 14, 2015 · N315AA · Boeing 767223SDR ABXA20150914181Support Fitting · corrodedFLAP SUPPORT NR 7, TENSION BOLT HOLE NR 4 HAS DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOCSep 14, 2015 · N315AA · Boeing 767223SDR ABXA20150914180Support Fitting · corrodedFLAP SUPPORT NR 7 TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOCSep 14, 2015 · N315AA · Boeing 767223SDR ABXA20150914176Support Fitting · corrodedNUMBER 8 FLAP SUPPORT TENSION BOLT HOLE NR 1, HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .672, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-44, PART NAME, FLAP SUPPORT FITTING NR 8, WSSep 14, 2015 · N315AA · Boeing 767223SDR UHLA201508290750Hinge · damagedINBD SPOILER OTBD HINGE NR 4, DRILL START ON TOP OF HINGE ON 2H WING SPAR. R & R INBD SPOILER OTBD HINGE IAW SRM 51-43-01. MAJOR REPAIR.Aug 29, 2015 · N861RW · Emb ERJ170100SESDR FDEA201508192624Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORRODED. SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0319684 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192623Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORRODED. BUSHING FABRICATED & INSTALLED IAW EA 1-57-50-T0319684 PART 1 STEP 1D. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192622Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORRODED. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0319684 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192621Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORRODED. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0319684 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192620Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORRODED. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0319684 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192619Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR HOLE OTBD BORE CORROSION. FOUND OUT OF LIMITS IAW CMM 57-44-09. FABRICATED A BUSHING & INSTALLED IAW EA 1-5750-T0319684 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192618Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR HOLE INBD BORE CORROSION. FOUND OUT OF LIMITS IAW CMM 57-44-05. FABRICATED BUSHING & INSTALLED IAW EA 1-5750-T0319684 PART 1 STEP 1C. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192616Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT HOLE INBD BORE CORRODED. BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319687 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192615Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD HINGE, WING SIDE, LOWER MOUNT HOLE INBD SURFACE CORRODED. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0319687 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192614Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT HOLE OTBD SURFACE CORRODED. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0319687 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508192613Hinge Bracket · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER MOUNT, OTBD HOLE BORE CORRODED. BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0319687 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 19, 2015 · N631FE · Doug MD11FSDR FDEA201508172596Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.205", FINAL HOLE DIAMETER 1.223", MAX ALLOWABLE DIAMETER 1.220". BUSHING FABRIAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172595Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 1.253", FINAL HOLE DIAMETER 1.258", MAX ALLOWABLE HOLE DIAMETER 1.254". OVERSIAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172594Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.704", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". SHOUAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172593Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 0.703", FINAL HOLE DIAMETER 0.723", MAX ALLOWABLE HOLE DIAMETER 0.709". SHOAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172592Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION AT HOLE 4 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER 2.311", FINAL HOLE DIAMETER 2.318", MAX ALLOWABLE HOLE DIAMETER 2.3135". OVERSIZED BUSHIAug 17, 2015 · N631FE · Doug MD11FSDR FDEA201508172591Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-08. EXISTING THICKNESS UPPER 0.376", LOWER 0.376", MATERIAL REMOVED UPPER 0.007", LOWER: 0.007", REMAINING THICKNESS UPPER 0.369", LOWER 0.369Aug 17, 2015 · N631FE · Doug MD11F
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