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 FDEA201202170602Bushing · corrodedRT WING, FLAP SIDE INBD FLAP HINGE INBD PIVOT HOLE BUSHING WORN. REPAIRED AS PER EA#1-5750-159802. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 114.SDR FDEA201202120557Bushing · corrodedLEFT WING - WING SIDE FLAP OTBD HINGE, OTBD ACTUATOR HOLE FOUND CORROSION. REWORKED IAW EA 1-5750-76015A. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76015A . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. EXISTING HOLE DIA 1.222" FINAL HOLE DIA SDR FDEA201202120556Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. EXISTING HOLE DIAMETER 1.222", FINAL HOLE DIAMETER 1.253", MAX HOLE DIAMETER 1.220". BUSHING FABRICATED AND INSTALLED IAW EA1-5750-76015A PART 2, SSDR FDEA201202120555Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. UPPER EXISTING THICKNESS;0.401" MATERIAL REMOVED: 0.002" REMAINING THICKNESS : 0.399" LOWER EXISTING THICKNESS : 0.417" MATERIAL REMOVED: 0.00SDR FDEA201202120554Hinge Fitting · corrodedLEFT WING, WING SIDE, OTBD FLAP, OTBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A, STEP 3 AND 4 PART 2. INBD EXISTING THICKNESS :0.416" INBD FWD MATERIAL REMOVED :0.002" REMAINING THICKNESS:0.414" OTBD EXISTING THICKNSDR FDEA201202120553Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP OTBD HINGE LOWER MOUNT AFT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. INBD AFT EXISTING THICKNESS;0.414" MATERIAL REMOVED : 0.008" REMAINING THICKNESS : 0.406" OTBD AFT EXISTING THICKNESS : 0.399" MATERIAL REMOVED:SDR FDEA201202120552Bushing · wornLEFT WING, WING SIDE OTBD FLAP INBD HINGE ACTUATOR HOLE OTBD HOLE BUSHING WORN OUT. REPAIRED IAW EA 1-5750-76665A, PART 2, STEP 6. EXISTING HOLE DIA 1.221" MAX. ALLOWABLE HOLE DIA 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76665A. REPAIR SDR FDEA201202120551Bushing · wornLEFT WING, WING SIDE OTBD FLAP INBD HINGE ACTUATOR HOLE INBD HOLE BUSHING WORN OUT. REPAIRED IAW EA1-5750-76665A, PART 2, STEP 6. NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-76665A, PART 2, STEP 6. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202120550Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP INBD HINGE LOWER MOUNT FWD AND AFT SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-76665A, STEP 3 AND 4 PART 2. INBD EXISTING THICKNESS :0.447" INBD FWD MATERIAL REMOVED:0.008" REMAINING THICKNESS: 0.439" OTBD EXISTING THICKNESDR FDEA201202120549Hinge Fitting · corrodedLEFT WING, WING SIDE OTBD FLAP INBD HINGE LOWER MOUNT AFT SURFACE FOUND CORROSION. REPAIRED IAW EA 1-5750-76665A PART 2, STEP 3 AND 4. OTBD AFT EXISTING THICKNESS :0.439", MATERIAL REMOVED 0.015", REMAINING THICKNESS 0.424". INBD AFT EXISTING THICKNESS :0.4SDR FDEA201202120548Bushing · wornLEFT WING, WING SIDE OTBD FLAP INBD HINGE PIVOT HOLE BUSHING WORN OUT. REPAIRED IAW EA1-5750-76665A PART 2. NEW BUSHING FABRICATED AND INSTALLED IAW EA1-5750-76665A PART 2, STEP 6 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202090531Hinge Fitting · corrodedRT WING, WING SIDE OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. CORROSION REMOVED IAW CMM 20-11-02, REV 72. EXISTING THICKNESS :0.434" MATERIAL REMOVED :0.002" REMAINING THICKNESS : 0.432". FOUND WITHIN LIMITS IAW DWG ARC0502 SHEET 4, SDR FDEA201202090530Bushing · wornRT WING WING SIDE OTBD FLAP, INBD HINGE PIVOT HOLE BUSHING WORN OUT. R & R WITH NEW BUSHING IAW EA 1-5750-76664A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201201030010Hinge Fitting · crackedLT WING, OTBD FLAP, INBD FWD HINGE FITTING (OTBD HALF), SUSPECT CRACK. INSTALLED NEW HINGE FITTING IAW DWG NR 6013.SDR FDEA201109013616Hinge Bracket · corrodedLEFT WING, OTBD FLAP, INBD HINGE (WING SIDE) STA XW 486.403, ACTUATOR OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS MER CMM 57-44-08 REV 70. ORIGINAL DIAMETER = 1.2055 INCH; MAX ALLOWABLE DIAMETER =1.220 INCH; FINAL DIAMETER = 1.250 INCH.SDR FDEA201109013615Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) STA XW 486.403, ACTUATOR INBD HOLE FOUND CORRODED. (HOLE SIZE EXCEEDED LIMIT). REWORKED AND FOUND EXCEEDED LIMIT AS PER SRM CMM 57-44-08 REV 70. ORGINAL DIAMETER = 1.2035 INCH; MAX ALLOWABLE DIAMETER = 1.220 INCH; SDR FDEA201108293547Hinge Bracket · corrodedRT WING OTBD FLAP INBD HINGE (WING SIDE) WING STA XW 486.403, LOWER MOUNT OTBD HOLE FOUND CORRODED HOLE EXCEEDED CMM 57-44-08 LIMITS ARC 0502-14. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-154210, & EO 1-5750-7-5002. REPAIR CLASSIFIED AS MAJOR SDR FDEA201107272996Hinge · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) BARREL NUT SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-150758, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201107272995Hinge · corrodedLT WING OTBD FLAP, INBD HINGE (WING SIDE) ACTUATOR OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.217", FINAL DIAMETER = 1.256", MAXIMUM ALLOWABLE DIAMETER = 1.220". REPAIR BUSHING AND WASHERS FASDR FDEA201107272994Hinge · corrodedLT WING OTBD, FLAP INBD HINGE (WING SIDE) ACTUATOR MOUNT FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.216", FINAL DIAMETER = 1.257", MAXIMUM ALLOWABLE DIAMETER = 1.220". REPAIR BUSHING AND WASHER FABRICSDR FDEA201107262956Hinge · corrodedLT WING OTBD FLAP INBD HINGE (WING SIDE) FORWARD MOUNT FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.188", FINAL DIAMETER = 1.263", MAXIMUM ALLOWABLE DIAMETER =1.254". REPAIR BUSHING FABRICATED AND INSTASDR FDEA201107262955Hinge · corrodedLT WING OTBD FLAP, INBD HINGE (WING SIDE) FORWARD MOUNT INBD HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.186", FINAL DIAMETER = 1.263", MAXIMUM ALLOWABLE DIAMETER =1.254". REPAIR BUSHING FABRICATESDR FDEA201107262952Hinge · corrodedLT WING OTD FLAP, OTBD HINGE (WING SIDE) ACTUATOR INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 70. ORIGINAL DIAMETER = 1.212", FINAL DIAMETER = 1.250", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING FABRICATED AND ISDR FDEA201107212877Hinge · corrodedRT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.206", FINAL DIAMETER = 1.250", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING AND WASHER FABRSDR FDEA201107212876Hinge · corrodedRT WING OTBD FLAP, INBD HINGE (WING SIDE) ACTUATOR INBD HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 70. ORIGINAL DIAMETER = 1.206", FINAL DIAMETER = 1.255", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING AND WASHER FABSDR IXXA11SMN083SSupport Fitting · crackedDURING ROUTINE C-CHECK INSP, FOUND RT WING FLAP LINK SUPPORT LT SIDE CRACKED AT STA XF 409.000. REMOVED HINGE CRACKED SUPPORT FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW HINGE SUPPORT FITTING IAW S/B 27-249, REV 1, SRM 51-3-0, SRM 51-1-21, SRM SDR FDEA201106022094Hinge Fitting · corrodedRT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA1-5740-147656. EXISTING HOLE: 2.252" FINAL HOLE: 2.3185" MAX HOLE: 2.3135" . NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5740-147656. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-SDR FDEA201106022093Hinge Fitting · corrodedRT WING OTBD FLAP INBD HINGE (WING SIDE) SIDE LINK HOLE FOUND SURFACE CORRODED. REWORKED IAW CMM 20-11-02, REV 70. UPPER FACE EXISTING THICKNESS 0.481", MATERIAL REMOVED 0.003", REMAINING THICKNESS 0.478", LOWER FACE EXISTING THICKNESS 0.486" MATERIAL REMOVESDR FDEA201106022092Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDE LINK HOLE, FOUND SURFACE CORRODED. REWORKED IAW EA 1-5740-147651. EXISTING THICKNESS 0.3845", MATERIAL REMOVED 0.003", REMAINING THICKNESS 0.3815". REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.SDR FDEA201106022091Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD HINGE (WING SIDE) SIDE LINK HOLE SPOT FACE, FOUND CORRODED. REPAIRED IAW EA 1-5740-147655. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201106022090Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDE LINK HOLE SPOT FACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 70. REMOVED: 0.003", FOUND THE REMAINING THICKNESS OF 0.460" AND 0.464" IS WITHIN DWG ARC 503 SHEET 2 BG LIMITS AND CMM 57-44-09 REV 70 FIG.SDR FDEA201106022089Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) LOWER INBD MOUNT HOLE SPOT FACE FOUND CORRODED. REPAIRED IAW EA 1-5740-147654. EXISTING THICKNESS: 0.439", MATERIAL REMOVED: 0.003"(FWD), MATERIAL REMOVED: 0.050"(AFT). REMAINING THICKNESS : 0.386",MINIMUM THICKNSDR FDEA201106022088Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) UPPER OTBD MOUNT HOLE FOUND CORRODED. REWORKED IAW EA 1-5740-147654, PART 1(B). EXISTING HOLE: 0.881", FINAL HOLE: 0.947", MAX.HOLE: 0.944". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5740-147654, PART 1(B). SDR FDEA201106022087Hinge Fitting · corrodedLEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) PIVOT HOLE FOUND CORRODED. REWORKED IAW EA 1-5740-147654 PART 1 A. EXISTING HOLE 2.251", FINAL HOLE 2.352", NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5740-147654, PART 1 A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-1SDR DALA1133029875Hinge · wornRT WING, STA XRS 353, T/E FLAP HINGE BUSHING WORN. REMOVED AND REPLACED RT WING FLAP HINGE IAW AMM 57-40-01-201-925A AND AMM 20-16-00-401-926A-A. REMOVED CABLE BLOCKS ON AILERON RT CTRL CABLES AND TRIM CABLES IAW AMM-57-40-01-201-925A AND AMM-27-10-00-501-9SDR FDEA201104261628Bracket · crackedCRACK INDICATION FOUND APPROXIMATELY 0.2 INCH IN LEGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON CENTER HINGE OF RIGHT WING NR 1 SPOILER INBOARD LUG. RIGHT WING NR 1 SPOILER CENTER HINGE BRACKET REMOVED AND REPLACED AS PER EO 6-5710-7-3307 EOCN 04 PART SDR FDEA201104261627Bracket · crackedCRACK INDICATION FOUND APPROXIMATELY 0.2 INCH IN LEGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON CENTER HINGE OF LEFT WING NR 1 SPOILER OUTBOARD LUG. LEFT WING NR 1 SPOILER CENTER HINGE BRACKET REMOVED AND REPLACED AS PER EO 6-5710-7-3307 EOCN 04 PARTSDR FDEA201104031303Hinge Fitting · corrodedRT WING STA XW 638.3059 OTBD FLAP, OTBD FWD HINGE BARREL NUT FITTING SURFACE FOUND CORRODED. RT WING OTBD FLAP OTBD FWD HINGE BARREL NUT FITTING SURFACE REWORK IAW CMM 20-11-02, REV 69 FOUND WITHIN LIMITS IAW DWG ARC0503, SHT 2, REV BG AND CMM 57-44-09, FIG 6SDR FDEA201104031302Hinge Fitting · corrodedRT WING STA XW 486.403 OTBD FLAP INBD FWD HINGE ACTUATOR OTBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149729. WINGS - FLIGHT SURFACES - RT WING FWD OTBD FLAP INBD HINGE - (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201104031301Hinge Fitting · corrodedRT WING, STA XW 486.403 OTBD FLAP INBD FWD HINGE ACTUATOR INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149729. WINGS- FLIGHT SURFACES- RT WING FWD OTBD FLAP INBD HINGE - (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201104031300Hinge Fitting · corrodedRT WING OTBD FLAP INBD FORWARD HINGE AT STA XW 486.403 BARREL NUT FITTING SURFACE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149729 WINGS-FLT SURFACES-RT WING FWD OTBD FLAP INBD HINGE-(WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201103291219Hinge Fitting · corrodedLT WING OTBD FLAP, INBD FWD HINGE BARREL NUT FITTING SURFACE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149730, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR CA110315014Hinge Fitting · cracked(CAN) DURING ACCOMPLISHMENT OF AD 80-12-10 R1/SB 57-55 THE LEFT OUTBOARD HINGE UPPER LUG WAS FOUND TO BE CRACKED.SDR KCSA111047Hinge Fitting · gougedNR 10 SPOILER, INBOARD NR 1 HINGE FITTING ON WING IS GOUGED.SDR FDEA201011174408Support · crackedLEFT OTBD FLAP INBD HINGE-FWD FITTING ATTACHED TO THE WING HAS A CRACK ON INBD SIDE. REMOVED CRACKED SUPPORT FITTINGS IAW SRM 51-33-01. WORKED HOLES TO FINAL SIZE .325 ON OTBD FLALP SUPPORT FITTINGS COMPLIED WITH EA 8-5710-125587 FOR MISLOCATED HOLE REPAIR. SDR FDEA201011124323Hinge Fitting · corrodedRT WING OTBD FLAP OTBD HINGE FITTING, LOCATION NR 3 FWD MOUNTING SURFACE CORRODED. ACCOMPLISHED REPAIR OF THE NR 3 MOUNT SURFACE OF THE OUTBD FLAP OUTBD HINGE FITTING IAW EA 8-5750-123566.SDR FDEA201010053930Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 51. FOUND WITHIN DAC DWG ARC0503, SHEET 2, REV BG LIMIT AND CMM 57-44-09, REV 51, TABLE 601 IN-SERVICE REWORK LIMIT. SHIM FABRICATED SDR FDEA201010053929Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201010053928Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201010053927Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.
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