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.
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
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 AALA20151015006Support Fitting · crackedRIGHT WING, GND SPOILER ACTUATOR SUPPORT FITTING CRACKED AT FWD INBD CHAMFER. REPLACED RT WING GND SPOILER SUPPORT FITTING WITH NEW FITTING.SDR 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.SDR 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.SDR 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.SDR FDEA201510023041Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.SDR FDEA201510023040Hinge · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION.SDR FDEA201510013028Hinge · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION.SDR FDEA201510013027Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION.SDR FDEA201510013026Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION.SDR FDEA201510013025Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION.SDR FDEA201510013024Hinge · corrodedRIGHT WING OTBD FLAP FWD HINGE, WING SIDE, BARREL NUT HOLE BORE CORROSION.SDR FDEA201509303002Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE CORROSION.SDR FDEA201509303001Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION.SDR FDEA201509303000Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION.SDR FDEA201509302999Hinge · corrodedLEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION.SDR 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.SDR 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.SDR 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 DETASDR 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 DETASDR 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 & INSTSDR 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 & INSTSDR 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. REPSDR 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 DETAISDR 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 DETAISDR 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.SDR 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, SDR 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,SDR 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 LOCATISDR 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 SDR 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 LOCSDR 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 LOCSDR 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, WSSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 FABRISDR 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". OVERSISDR 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". SHOUSDR 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". SHOSDR 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 BUSHISDR 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 0.369
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