JASC 5744
Service difficulty reports · 2,731
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 03FDEA01189Hinge · corrodedSNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. CORRECTIVE ACTION: SNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS IAW EA 1-5750-71806, TITLE: WINSDR 03FDEA01216Hinge · corrodedRIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE CORRODED. RIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE REPAIRED AS PER FEDEX AE 1-5750-71880, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES- RT INBOARD FLAP OUTBOARDSDR 03FDEA01190Hinge · corrodedLEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. LEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69406, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVISDR 03FDEA01188Hinge · corrodedLEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORRODED. LEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 ANSDR DL76S030650Support Beam · corrodedWING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : CORROSION IN AFT ATTACH HOLE BORES. THE AFT 4 ATTACH HOLES FOR THE OUTBD SUPPORT BEAM AT THE INBD FLAP ATTACH LOCATION WERE FOUND CORRODED. THE HOLES WERE REAMED TO REMOVE CORROSION, HFEC INSPECTED, OVERSISDR DL76S030649Support Beam · corrodedWING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : FWD FLAP ATTACH HOLE CORROSION, THE 2 FWD FLAP ATTACH HOLES ON THE OUTBD SUPPORT BEAM NR 3 SUPPORT FOR THE INBD FLAP LOCATION WERE FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES, HFEC INSSDR 03FDEA01024Fitting · corrodedLEFT WING (WING SIDE) - OUTBOARD T/E FLAP, OUTBOARD HINGE FITTING FOUND HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORRODED. LEFT WING (WING SIDE) - OUTBOARD T/E FLAP, OUTBOARD HINGE FITTING HYDRAULIC ACTUATOR MOUNTING HOLE OUTBOARD SIDE CORROSION REPAISDR 03FDEA01013Hinge · corrodedLT WING - OUTBOARD T/E FLAP, OUTBOARD FWD HINGE FITTING FOUND OUTBOARD LOWER REAR SPAR ATTACH MOUNT HOLE WITH CORROSION (WING SIDE FITTING). REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69356 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP. OUTSDR AMTA200300903Attach Fitting · crackedRIGHT WING AFT SPAR OUTBOARD AILERON ATTACH FITTING CRACKED AT SECOND HINGE FROM OUTBOARD. REPLACED FITTING IAW SRM 51-10-01 AND ER/A L10-57R-5202. (M)SDR AUS20030580Fitting · cracked(AUS) RT WING INBOARD SPOILER MAIN ACTUATOR SUPPORT FITTING CRACKED IN THE OUTBOARD SUPPORT CHANNEL AND PASSING THROUGH THE SPOILER DOWNSTOP PAD FITTING REAR RIVET HOLE. FOUND DURING INSPECTION IAW MFG ALERT SB 717-57A0016.SDR 03FDEA00835Hinge Fitting · corrodedSNRM N0767: LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FWD FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR'S UPPER LT AND RT MOUNT HOLES WITH CORROSION (WING SIDE FITTING). SNRM N0767: REPAIR CARRIED-OUT IAW CMM 57-44-08 AND EA 1-5740-71706 WINGS - LEFT OUTSDR 03FDEA00837Hinge Fitting · corrodedSNRM N0746: RT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP-HINGE FWD FITTING FOUND INBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0746: REPAIR CARRIED-OUT AS PER CMM 57-44-08 AND FEDEX EA 1-5740-68424 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGSDR 03FDEA00838Hinge Fitting · corrodedSNRM N0750: RT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP-HINGE FWD FITTING FOUND INBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0750: REPAIR CARRIED-OUT IAW CMM 57-44-09 AND EA 1-5740-71708 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKSDR 03FDEA00839Hinge Fitting · corrodedSNRM N0748: RT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP-HINGE FWD FITTING FOUND OUTBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0748: REPAIR CARRIED-OUT IAW CMM 57-44-09 AND EA 1-5740-71708 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACSDR 03FDEA00840Hinge Fitting · corrodedSNRM N0769: LT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FWD FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR'S UPPER LUG MOUNT HOLES, LT AND RT WITH BORE SURFACE CORROSION (WING SIDE FITTING). SNRM N0769: REPAIR CARRIED-OUT AS PER CMM 57-44-09 AND FEDEX EA 1-5SDR DL767030437Support Fitting · corrodedTHE HOLE BORES FOR THE FLAP ATTACMENTS ON THE INBD SUPPORT FITTING ON THE LT INBD FLAP ON THE LT WING WERE FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES, HFEC INSPECTION, INSURANCE REAM, AND INSTALLATION OF ALUMINUM BUSHINGS PER ER/ASDR CA021108006Washer · mismanufactured(CAN) ANTI-ROTATION WASHER SHOWN IN IPC 57-26-13 FIG 01B ITEM 60 IS NOT MANUFACTURED INACCORDANCE WITH DRAWING. SHARP EDGE CUTOUT ON WASHER INTERFERES WITH RADIUS LUG ON FITTING-PREVENTS WASHER FROM LAYING FLAT ON THE ACTUATOR FITTING-PREVENTS BEARING FROM BESDR IXXA0200141SSupport · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE INBOARD AND OUTBOARD LOWER AREA OF THE NR 2 FLAP HINGE UPPER SUPPORT ON THE RIGHT WING. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOSDR LR7A02057Stiffener · crackedDURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND RH OWS 241 FLAP TRACK STIFFENER CRACKED.REPLACED STIFFENER IAW SRM SMP 583 57-50-03. NR 0106.SDR CA020529003Hinge · cracked(CAN) CRACK FOUND IN LOWER ATTACH FLANGE DURING SPECIAL INSPECTION PER CESSNA CONTINUED AIRWORTHINESS PROGRAM.THIS WAS LEFT HAND INBOARD HINGE. ALSO FOUND RIGHT HAND INBOARD HINGE CRACKED. OUTBOARD LEFT HAND HINGE HAD BEEN RECENTLY REPLACED.SDR QXEA0200160Attach Fitting · chafedPDX - LT WING STATION 8200 FLAP BEAM ATTACH FITTING ON REAR SPAR HAS TWO CHAFE MARKS ON BOTH LUGS OF FITTING. REPAIRED IAW HORIZON AIR EA 4-57-577 AND FOKKER SRM 51-10-04.SDR CA011205003Bushing · cracked(CAN) WHILE PREFORMING A FLAP SUPPORT INSPECTION, A CRACK WAS FOUND ON THE FLAP ROLLER BUSHING (LT REAR). THE CYLINDRICAL BUSHING WAS SPLIT IN HALF AND ONLY BECAME APPARENT WHEN THE BUSHING WAS REMOVED FROM THE FLAP ROLLER ASSEMBLY.SDR AALA20014069Beam · corrodedAFW - RIGHT INBOARD FLAP SUPPORT BEAM (9-10 BEAM ASSY) HAD THE MOST OUTBOARD FLAP ATTACH HOLE REAMED TO .503 TO REMOVED CORROSION. OVERSIZE HOLE TO REMOVE CORROSION AND VISUALLY INSPECT THE BORE TO ENSURE CORROSION REMOVAL. FABRICATED REPAIR BUSHING. INSTALSDR 01FDEA00939Attach Fitting · out of positionRT WING INBOARD FLAP OUTBOARD HINGE ATTACH FITTING TO REAR WING SPAR MIGRATED. REMOVED AND REPLACED PER DWG ARB0621 & MM 27-50-20-4.SDR AUS20011107Bracket · cracked(AUS) INBOARD AILERON BRACKET BROKEN INTO TWO PIECES.SDR 01FDEA00817Rib · crackedN 1494 LH WING L/E RIB CRACKED FOR ACTUATOR ROD END CUT-OUTS FOR #2 SLAT AT WS 640, WBL 540. R&R RIBS PER SRM 57-30-4.SDR HNAA0100060Track · corrodedL/H WING #3 FLAP TRACK HAS AREA OF CORROSION ON BACK FACE OF TRACK. BLENDED CORROSION IAW EO8-57-01-396.SDR HNAA010061Track · corrodedR/H WING #3 FLAP TRACK HAS CORROSION ON BACK SURFACE. BLECDED CORROSION IAW EO8-57-01-396.SDR HNAA0100051Bracket · crackedAILERON CONTROL QUADRANT MOUNTING BRACKET ON L/H WING REAR SPAR FOUND CRACKED AT OUTBOARD END OF THE LOWER FLANGE TO 1/16" BEYOND THE FIRST RIVET HOLE. REPAIRED IAW ESR8-57-01-012A.SDR 0102772710Hinge Fitting · corrodedDuring "M" check found corrosion on LH inboard aileron hinge fitting. Repaired per EA 27-184387.SDR 2001F00109Bracket · crackedCRACKED AT AILERON YOLK ATTACH POINTS.SDR COOSDR010032Support · crackedLEFT WING AILERON, SUPPORT ASSY PN 65-21776-7 LUG CRACKED.SDR C2XA01BT108Attach Fitting · faultyYUL---DURING 2C INSPECTION MAINTENANCE FOUND FAULTY TRAILING EDGE ATTACH BRACKETS. REPAIRED THE UPPER SURFACE TRAILING EDGE ATTACHMENT FITTINGS IAW ATR42 SRM 57-50-00 FIGURE 402.SDR QXEA0100767Support · damagedYYC - RIGHT-HAND INBOARD FLAP A-FRAME SUPPORT ASSEMBLY HAS OVER SIZED BORES IN AFT 3 ATTACH HOLES. OVERSIZE HOLES REAMED TO .3125 MIN FOR 5/16 BOLT AS PER FOKKER SRM 51-32-01, PAGE 11, TABLE 6. BOLTS INSTALLED PER FOKKER FAX TS01.54655 AND HORIZON AIR EA 4-5SDR ABXA010077Stud · brokenLEFT FLAP OUTBOARD FLAP HINGE FITTING, OUTBOARD LOWER SPAR ATTACH STUD WAS BROKEN. MAINTENANCE INSPECTED AND REPLACD 4 OUTBD FLAP HINGE STUDS IAW DC-9 MM 57-118, 57-40-01 AND SERVICE SKETCH 2673.SDR UPS01235273Attach Fitting · crackedINSPECTION TYPE:C+SI, RT WING - CRACK AT NR 7 FLAP TRACK ATTACH AREA O/B FASTENER ROW, THIRD HOLE FROM FRONT. REPAIR CARRIED OUT IAW SRM 51-30-5 & SMRO WO 2001-006-013 UPS ENGINEERING FILE NR B727-5730-14010-A.SDR C2XA01TY020Attach Fitting · gougedTYS - DURING A SCHEDULED 1C INSPECTION, THE RIGHT AILERON INBOARD ATTACH BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE BLENDED AND DYE PENETRANT THE ATTACH BRACKET IAW EMB REF GST 0421/01, ALODINED AND PRIMED AREA IAW EMB 145 CMP 51-21-03, 51-21-04 AND 51-21-06SDR EISA20010011Attach Fitting · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACKS AT TOP OF LEFT WING AT NR 2, 3, AND 4 SPOILER ATTACH POINTS. STOP DRILLED CRACKS, FABRICATED, INSTALLED, ALODINED, AND PRIMED REPAIR DOUBLERS, IAW SRM 51-10-2, 51-30-4 FIG 10, AND 51-30-2.SDR EISA20010006Support Fitting · damagedDURING ROUTINE C-CHECK INSPECTION FOUND OUTBOARD TRACK SUPPORT HAS ELONGATED HOLE. REAMED FITTING IAW SB 57-0134, ALODINED AND PRIMED IAW SRM 51-10-2.SDR ERKR200100061Fitting · misdrilledTHIS REPAIR OF MISS-DRILLED HOLE DAMAGE TO RHS WING # 1 SLAT OUTBOARD FITTING P/N 9919301-2 AT STATION XIS 137.921. CONSISTS OF PLUGGING THE DISCREPANT MISS-DRILLED HOLES AND INSTALLING A REINFORCEMENT FITTING. PER ECRA 933-57-096-2.SDR UPS02237505Support Fitting · corrodedINSPECTION TYPE:C+SI LT WING SUPPORT BRACKET FOR NR 3 FLAP TRACK FWD END HAS PITTING CORROSION ON RT FACE OF LUG.SDR TWAA0018615Casting · corrodedDURING CHECK-C MAINT ON LT WING THE O/B FLAP I/B MOUNT CASTING ON SPAR TOP I/B STUD WAS EMITTING RUST. REPLACED 2 UPPER STUDS AND INSTALLED NEW HINGE CASTING PER MM 57-40-01.SDR 20001120SH013Flap Track · corrodedFOUND DURING C-CHECK, NR 4 AND NR 5 FLAP TRACK MOUNTING PAD MATING SURFACES/BOLT HOLES, CORRODED. SERVICE ORDER NR 109003 OPS NR 20507 AND 2062D TIMCO RED NR S00307. HOLE EXCEEDED THE LIMITS PER SB 727-57-0178 REV PARA B AND PARA H PART IV AND FIG 3, REF/B/.SDR AALA20001589Flap · corrodedTUL - CORROSION ON GROUND ATTACH BOLT AT NR 2 LEADING EDGE FLAP, OUTBOARD. INSTALLED DOUBLER PER ESO 11697 DATED 9-14-00. (X)SDR AU000777Fitting · loose(AUS) RIGHT AILERON FOULING ON UPPER WING SKIN PREVENTING FULL AILERON MOVEMENT. FURTHER INVESTIGATION FOUND THAT THE INBOARD HINGE ATTACHMENT BRACKET WAS NOT SECURED. THE TWO LOWER ATTACHMENT SCREWS WERE INSTALLED BUT NOT SECURED TO THE ANCHOR NUTS. (X)SDR HNAA0000052Bracket · crackedFOUND TWO CRACKS IN THE LOWER LEG OF THE LT AILERON INPUT QUADRANT BRACKET AT STATION YW417.9. REPAIRED BRACKET IAW EO8-57-00-687.SDR CALA0000670Support Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING O/B HINGE I/B FLAP SUPPORT. A NEW SUPPORT WAS INSTALLED IAW DOUGLAS DRAWING ARC2594-3 AND SRM 51-33-01.SDR TWAA0006601Casting · crackedDURING OP 16 MAINT CHECK, THE LT WING T/E NR 4 AILERON HINGE CASTING WAS CRACKED IN AFT MOUNT CLIP FOR WING T/E, TOP PANEL. REPLACED CRACKED BRACKET WITH NEW BRACKET USING NON MAGNETIC ATTACHMENTS PER SPM 6-70-01 AND FASTENER INSTALLATION PER SRM 51-30 AND SRSDR 00FDEA00174Attach Fitting · corrodedDURING ROUTINE INSP, THE LEFT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2.SDR 00FDEA00173Attach Fitting · corrodedDURING ROUTINE INSP, RIGHT O/B AILERON, I/B ATTACH FITTING WAS FOUND TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED PER IAW MM 27-10-031-2.
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