JASC 5753
Service difficulty reports · 31,515
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 06FDEA03271Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD MID BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD MID BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGS - SDR 06FDEA03270Bracket · corrodedRIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT INBOARD MID BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT INBOARD MID BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGSSDR USAA061159Skin · wornLT OB FORE FLAP OB END WORN. INSTALLED REPAIR DOUBLER IAW SRM 57-53-01, DEFECT SIZE: .25 X .50 INCH.SDR UPS06447998Skin · puncturedRT OB FLAP LWR SKIN APPX 1 INCH PUNCTURE. REMOVED DAMAGED AREA OF SKIN AND CORE PER SRM 51-40-06. DAMAGE REMOVED OKAY TO INSTALL REPAIR. DRYED AREA-INSTALLED REPAIR CORE AND STARTED CURE PER SRM 51-40-20. COMPLETED REPAIR PER SRM 51-40-20. REF LOG PAGE 566736SDR SWAA063463Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR CA061108005Bracket · cracked(CAN) FLAP SLAT BRACKETS CRACKED AT RADIUS. (TC NR 20061108005)SDR IXXA06SMN296SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP EXISTING UPPER SKIN DOUBLER IMPROPER AT STATION, XW38.000. REMOVED EXISTING SKIN WITH EXISTING IMPROPER REPAIR. FABRICATED NEW SKIN WITH AL 2024 T3 0.025” AND BONDED DOUBLER AL 2024 T3 0.020”. BONDSDR IXXA06SMN295SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING IB FLAP EXISTING LOWER. SKIN DOUBLER IMPROPER FROM STATION XW2.000 TO XW91.000. REMOVED EXISTING SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED ARESDR QXEA200602545Flap Track · corrodedC4 YYC - LEFT NR 1 FLAP TRACK UPPER FLANGE LOWER SURFACE HAS PITTING CORROSION. REPAIRED IAW RD8-57-985.SDR ASAA0680959Skin · crackedRIGHT WING OUTBOARD FLAP TRAILING EDGE IS CRACKED. REMOVED DAMAGED AREA. APPLIED FOUR REPAIR PLIES PER SRM 51-70-1.SDR ASAA0680958Vane · chafedRIGHT WING INBOARD FLAP INBOARD VANE IS CHAFED ON LEADING EDGE. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 57-03.SDR DLM88070402Vane · misrepairedEXISTING EXTERNAL REPAIR DOUBLER OUT OF SRM ON L/E OF RT WING OUTBD FLAP, INBD VANE AT STA 153.00. REMOVED EXISTING REPAIR AND INSTALLED REPAIR IAW AEROMEXICO DRAWING AMR0957141 R03 AND REPAIR SKETCH SK-06-147/AQR. APPROVED BY DELTA ERA 457403-14, STA XV1=153SDR DLM88070401Vane · delaminatedDELAMINATION ON EXTERNAL SKIN AND INTERNAL DOUBLER OF LT WING OUTBD FLAP INBD VANE. AN AREA 1.25 IN BY 2.0 IN AT EXTERNAL UPPER SKIN AND AN AREA 0.75 IN BY 1.25 IN AT INTERNAL DOUBLER FLAP VANE INBD END AT STA XV=153.00. REPAIRED PER AEROMEXICO REPAIR DRAWINSDR HALA0600755Skin · delaminatedL/E DELAMINATED ON LEFT WING O/B FLAP 7 INCHES FROM I/B END. REPAIRED THE L/E DELAMINATION ON THE LEFT WING OUTBOARD FLAP 7 INCHES FROM THE INBOARD FWD SRM 57-53-01/101 AND SRM 51-70-17-0G-0 AND AMM 51-21-10-307-020.SDR UPS06848004Brace · corrodedINSPECTION TYPE:C3 L/H FLAP CANOE FITTING INBD SIDE BRACE STA 219 CORRODED AND PITTED OUT OF LIMITS. REMOVED AND REPLACED LT CANOE FITTING INBD SIDE BRACE AT STA 219 IAW SRM 57-2-00 FIG 6, AND DC8 MM 27-51-12-2.SDR SWAA063433Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.SDR QXEA200602490Skin · chafedC3 PDX - RIGHT FLAP HAS CHAFE DAMAGE ON UPPER SKIN OUTBOARD EDGE. REPAIRED IAW SRM 57-52-30, 51-25-10, AND SRM 51-25-15.SDR RAIA00609010Bearing · wornFLT NR 7938 - STL - AIRCRAFT BUFFETING IN FLIGHT, INSPECTED ON GROUND AND FOUND LEFT INBOARD FLAP BEARING LOOSE. MAINTENANCE REMOVED AND REPLACED THE LT OB FLAP INBOARD ROLLER BEARING.SDR TRAX200600734Arm · crackedPOSSIBLE CRACK ON RT OB FLAP NR 4 HINGE ARM FWD ATTACH POINT. LPI OR EDDY CURRENT INSPECTION REQUIRED FOR VERIFICATION. CRACKED AREA MARKED. (MTC) REMOVED AND REPLACED RIGHT OUTBOARD FLAP IAW CRJ200 AMM 27-54-05/JC7020945 (CLOSED)SDR DHL2006745537Wedge · delaminatedREF ASTAR N/R 55925. DISCREPANCY: RT O/B FORE FLAP SHOW DELAM SPOT T/E IB END, WBL 298. REMOVED END CAP AND REMOVED DAMAGED UPPER AND LOWER SKINS, CORE, AND WEDGE; FABRICATED REPAIR CORE, 2 EA SKINS AND 2 EA DOUBLERS. BONDED LOWER REPAIR SKIN, DOUBLER AND SDR QXEA200602546Flap Track · corrodedC4 YYC - LEFT WING NR 5 FLAP TRACK OUTBOARD LOWER HORIZ FLANGE UPPER SURFACE AND OUTBOARD VERTICAL FACE HAVE PITTING CORROSION, ALSO INBOARD LOWER HORIZ FLANGE UPPER AND LOWER CORNER SURFACES HAVE PITTING CORROSION. REPAIRED IAW RD8-57-989.SDR SWAA063381Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP TORQUE TUBE PER MM.SDR SWAA063380Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP TORQUE TUBE PER MM.SDR SWAA063360Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.SDR 2006FA0000942Flap Track · damagedDURING 200/600 HR PHASE INSPECTION FOUND THE RT IB AFT FLAP TRACK UPPER 3 ATTACH FASTENERS PN: MS90354S0609 WORKING. RECOMMEND ADDITIONAL ATTENTION TO FLAP RIGGING AND ALL ATTACHING HARDWARE DURING PHASE INSPECTION. (K)SDR 2006FA0000941Flap Track · damagedDURING 200/600 HR PHASE INSPECTION FOUND THE RT IB AFT FLAP TRACK UPPER 3 ATTACH FASTENERS PN: MS90354S0609 WORKING. RECOMMEND ADDITIONAL ATTENTION TO FLAP RIGGING AND ALL ATTACHING HARDWARE DURING PHASE INSPECTIONS. (K)SDR ABXA060264Skin · corrodedSURFACE CORROSION FLAP OB LEADING EDGE LOWER SURFACE. REPAIRED AREA IAW SRM 57-01.SDR UPS06847990Fitting · crackedINSPECTION TYPE:C3 RT FLAP STA 3 FITTING CRACKED. REMOVED RT FLAP FITTING AT STA 3 IAW 51-1-21. LOCATED, DRILLED UP REPLACEMENT FITTING AND INSTALLED AT RT FLAP STA 3 IAW SRM 51-3- 2, 51-1-21A.SDR SWAA063344Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR ASAA0640948Skin · damagedLEFT OUTBOARD MIDFLAP UPPER SURFACE CHAFED AT OUTBOARD END. LEFT OUTBOARD MIDFLAP UPPER SURFACE REPAIRED IAW SRM 51 70 10 REPAIR 4.SDR ASAA0640947Skin · chafedLEFT OUTBOARD MIDFLAP L/E CHAFED AT INBOARD END. LEFT OUTBOARD MIDFLAP L/E CHAFED AREAS AT INBOARD END REPAIRED AND MADE SERVICEABLE ON WING AND ADJUSTMENT CHECK CARRIED OUT AND FOUND SERVICEABLE IAW SRM 57 53 01 AND AMM 27 51 34 501.SDR ASAA0640946Skin · chafedLEFT INBOARD MIDFLAP UPPER SURFACE INBOARD EDGE SKIN CHAFED. LT INBOARD MIDFLAP UPPER SKIN CHAFED AREAS REPAIRED ON WING AND MADE SERVICEABLE AND GAP CHECK CARRIED OUT FOUND SERVICEABLE IAW SRM 57 53 01 AND AMM 27 51 04 401.SDR ASAA0680943Vane · corrodedLEFTHAND OUTBOARD FLAP CENTER VANE CORRODED AT XV2 288 292. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.SDR ASAA0680942Vane · gougedLEFTHAND OUTBOARD FLAP INBOARD VANE L/E GOUGED AT XVI 153 160. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.SDR ASAA0680941Vane · dentedLEFTHAND INBOARD FLAP INBOARD VANE DENTED AT XIVIF 6 35. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.SDR ASAA0640939Skin · chafedLEFT INBOARD T/E FLAP EXHAUST GATE UPPER SKIN IS CHAFED AT FWD O/B CORNER. REPLACED EXHAUST GATE IAW AMM 27-51-05.SDR ASAA0640938Skin · dentedRIGHT INBOARD AFT FLAP L/E SKIN DENTED. REPLACED DENTED SKIN WITH FABRICATED REPAIR PARTS IAW SRM 50-30-01 AND 51-40-02.SDR CA061109005Bracket · cracked(CAN) IB FLAP P/N 13760B463, SLAT BRACKETS P/N 137204B51 AND 137205B67 FOUND CRACKED AT BEND RADIUS. REMOVED AND REPLACED WITH NEW. (TC NR 20061109005)SDR 06FDEA03181Skin · damagedEXISTING REPAIR FOUND ON RHW I/B FLAP ASSY UPPER SURFACE O/B SEGMENT.SDR 06FDEA03180Skin · damagedEXISTING REPAIR FOUND ON RHW I/B FLAP ASSY LWR SURFACE, 63" FROM O/B, 31" FROM T/E.SDR 06FDEA03179Skin · dentedLHW I/B FLAP ASSY O/B SEGMENT LWR SURFACE FOUND MULTIPLE DENTS. LT WING I/B FLAP ASSY O/B SEGMENT LOWER SURFACE MULTIPLE DENTS REPAIRED AS PER SRM 57-10-00 FIG.2 VOL. I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.SDR LR7A06169Skin · corrodedDURING SCHEDULED B1 CHECK PER JOB CARD HB2703, FOUND LT OUTBOARD BOTTOM FLAP SKIN CORRODED AND BULGING AT FLPS 190. REPAIRED SKIN IAW LAC MEA 382-27-06-084.SDR 06FDEA03167Hinge Fitting · corrodedDURING FLAP REPLACEMENT RT WING O/B FLAP O/B HINGE FITTING P/N ARC1991 I/B FWD BOLT HOLE FOUND CORRODED. REPAIR CARRIED OUT AT RH WING O/B FLAP O/B HINGE FITTING I/B FWD BOLT HOLE AS PER FEDEX EA 1-5750-103507, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100SDR MALA060543Spar · crackedTHE REAR SPAR OF THE LT FLAP, P/N 7257800-503, S/N 1148, AT WS 142, IS CRACKED IN THE RADIUS OF THE LOWER SPAR CAP ANGLE. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO S57007. REF: EAMS WORK ORDER 214376 TASK 5512.SDR AWXA200601584Flap · debondedMCN - DISBOND AREA AT AFT INBD CORNER OF RT OUTBD AFT FLAP. REPAIRED DISBONDED AREA AT AFT INBD CORNER OF RT OUTBD AFT FLAP IAW B737-300, SRM 57-70-10-2R, REPAIR NR 4, FIG 202.SDR DHL2006805503Skin · dentedRT WING INBD FLAP DENTED XW 106.000 (UPPER SKIN) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1 PG 2. REMOVED PLATING DIAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 1 PG 2 ITEM "D". CLEANED, TREATESDR HALA0600889Skin · gougedRT WING IB T/E FLAP, L/E BULLNOSE GOUGED LWR SURFACE JUST I/B OF O/B FLAP ATTACH FITTING. REPAIRED RT WING I/B T/E FLAP. L/E BULLNOSE JUST I/B OF O/B FLAP ATTACH FITTING PER ER NO. 06-3617, HAL M105# 597012.SDR HALA0600890Skin · chafedLT IB FLAP, OB L/E BULLNOSE LWR L/E CHAFED/DAMAGED 53.5" TO 58". REPAIRED AREA IAW ER NR 06-3616, CUSTOMER AUTHORIZATION HAL M105#597011.SDR HALA0600787Skin · dentedLT I/B AFT FLAP, UPPER SURFACE DENT DISBONDED 31.5" FROM I/B END, 6" FWD OF AFT EDGE. LT I/B AFT FLAP UPPER SURFACE DENT DISBONDED 32.5" FROM I/B END, 6" FWD OF AFT EDGE, REPAIRED IAW SRM 51-0-10-2R-0&3.SDR HALA0600718Channel · crackedR/W CRACKED CHANNEL IB END OB FLAP 7 INCHES FROM L/E OF CLOSE OUT PANEL. REMOVED CRACKED CHANNEL FROM R/W IB END OF OB FLAP IAW SRM 51-40-02.REPAIRED CHANNEL IAW SRM 51-70-11 FIG 1 STEPS 1-12. REPAIRED DOUBLER MATERIAL 2024-T3 .63 INCHES, LOT NR 709033. INSTA
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