JASC 5753
Service difficulty reports · 31,521
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 04FDEA03265Panel · delaminatedRIGHT WING PANEL ARC0613-502, UPPER TRAILING EDGE PANEL AT INBOARD END OF OUTBOARD FLAP DELAMINATED. RIGHT WING PANEL ARC0613-502 REPAIRED BY FABRICATING AND BONDING NEW OUTER SKINS, DOUBLER AND CORE IAW TPS 1001 REV E, DAC DWG ARC0613 AND FEDEX EA 8-5710-815SDR 04FDEA03263Roller · looseRIGHT WING LOWER FORWARD INBOARD FLAP LOAD ROLLER HAS EXCESSIVE LATERAL PLAY. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK LOWER ROLLER IAW FEDEX EA 8-5750- 81513, WING- INBOARD FLAP- INBOARD ROLLER TORQUE REQUIREMENT- CLARIFICATION.SDR 04FDEA03262Roller · wornRIGHT WING LOWER AFT LOAD ROLLER HAS WORN BEARING SURFACE, CHROME WORN ON INBOARD FLAP TRACK ATTACHMENT AREA. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK AFT LARGE LOAD ROLLER IAW FEDEX EA 8- 5750-81513.SDR 04FDEA03254Hinge Bracket · corrodedLEFT AND INBOARD FLAP OUTBOARD HINGE BOLT HOLE HAS AREA OF CORROSION. BOLT HOLE IS REPLACEMENT BOLT PART NUMBER 3D0031-8-90 STEP 23 OF FEDEX WIC E 8-5710-7-5005 PT1. REMOVED STOP FITTING IAW DAC DWG ARC0154, REMOVED OUTBOARD PANEL IAW MD10 SRM 51-31-01 VOL 2,SDR AWXA200401364Wedge · delaminatedMCN - MAJOR REPAIR - DURING 8-DAY CHECK ,THE LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 14" FROM OUTBOARD END, BETWEEN WBL 169 AND WBL 176. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WING INBOARD MID FLAP TSDR AWXA200401363Wedge · delaminatedMCN - MAJOR REPAIR - DURING 8-DAY CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE 26" FROM OUTBOARD END, BETWEEN WBL 153 AND WBL 157. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WING INBOARD MID FLAP SDR SWAA043458Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED LT T/E AFT FLAP PER SRM.SDR 04FDEA03239Vane · chafedWINGS, LT INBD FLAP REWORK OF CHAFED AREA ON VANE TE EXTRUSION. CLOSING ACTION ON 11/26/04, ON N/R S00022. COMPLIED WITH EA 8-5710-55415.SDR 04FDEA03238Bracket · corrodedWINGS, RT INBD FLAP REWORK OF TRACK/DRIVER BRACKET P/N ARC2761. CLOSING ACTION ON 11/27/04 ON N/R S00018. COMPLIED WITH EA 8-5754-55412.SDR 04FDEA03233Hinge · corrodedDURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON LT OUTBOARD FLAP HINGE SECTION STA XW 638 WITH OXIDATION WHERE CONTACT STUD BOLTS. ACCOMPLISH CORROSION REWORK AT LT OUTBOARD FLAP FWD OUTB'D HINGE SECTION IAW CMM 51-44-09.SDR 04FDEA03229Skin · wornDURING AIRPLANE CONVERSION FROM P-F/ACF, FOUND RT WING OUTBD FLAP UPPER SIDE. LEADING EDGE B/T STA XOF 775-759 HAVE SKIN WITH WEAR DEEP. REPLACED SKIN PANEL X SRM 51-33-01 PG 34-47 DWG ARC1560.SDR 04FDEA03220Fitting · crackedRIGHT HAND WING - OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. OUTBOARD FLAP REMOVED AND REPLACED AS PER ARM 51-33-01 VOL II AND DRAWING ARC4125.SDR 04FDEA03219Fitting · crackedLT HAND WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND DWG ARC4125.SDR 2004FA0000894Bellcrank · crackedBEFORE LANDING, PILOT SELECTED 10 DEGREES FLAPS & ACFT DRIFTED LT. ABORTED LANDING, RAISED FLAPS & DID A GO AROUND THINKING, THAT ONE OF THE MLG HAD NOT COME DOWN. AT THE 2ND ATTEMPT, HAD SAME PROBLEM & REALIZED THE PROBLEM WAS NOT THE MLG, BUT THE FLAP SYS.SDR ASAA0410607Skin · dentedOKC - DURING C-CHECK, LEFT OUTBOARD MID FLAP UPPER SURFACE HAS A DENT INBOARD OF NR 1 FLAP SPINDLE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-20. (M)SDR ASAA0410606Skin · dentedOKC - C-CHECK DENT WITH CREASE, CENTER OF LEFT INBOARD FORE FLAP, UPPER SURFACE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-20. (M)SDR ASAA0410568Skin · chafedOKC - FOUND LEFT WING TRAILING EDGE OUTBOARD MID FLAP HAS TWO CHAFED AREAS IN SKIN, LOWER SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW AS EA AND AAR EA. (M)SDR SWAA043426Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.SDR SWAA043425Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.SDR 04FDEA03193Hinge · corrodedRIGHT WING OUTBOARD FLAP, INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUSHING, FOUND OUT OF LIMITS. INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA NR 8-5750-83939, WING-RIGHT HAND OUTBSDR USAA041073Skin · delaminatedPIT - Q5 - SKIN, 4 INCH X 4 INCH AREA, DELAMINATION, AT IB AFT FLAP BOTTOM. REMOVED BOTTOM SKIN, CORE, INSTALLED BOTTOM REPAIR DOUBLER IAW SRM. (K)SDR SWAA043420Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT MID SPAR AREA. REMOVED FORE FLAP ASSY PER MM.SDR DHL2004755517Skin · gougedDURING A C-CHECK, LEFT WING I/B AFT FLAP - FORE FLAP HAS A GOUGE ON EXISTING EXTERNAL DOUBLER AT O/B END. CUT OUT EXISTING SKIN O/B FLAP IAW B727 SRM 51-10-1, FABRICATED SKIN 2020T3 .050 PO 9001425 7 X 12.5 INCH FILLER DOUBLER 2024T3.060 PO 9001387, 5.5 X 12.SDR CA050128007Hinge Bracket · damaged(CAN) LOOSE RIVETS ATTACHING CENTER FLAP HINGE BRACKET TO IB AND OB PORTIONS OF FORE FLAP ASSY. HIDDEN PROBLEM DOES NOT REALLY SHOW UP UNTILL YOU TAKE THE FLAP OFF. FORE FLAP DISASSEMBLED AND RIVETS REPLACED WITH NEW.SDR 04FDEA03171Skin · canningRIGHT INBOARD FLAP INBOARD AFT SEGMENT UPPER SURFACE HAS A LARGE SKIN SECTION OIL CANNING. REPLACED SKIN PNL ASSY IAW DC-10 SRM 51-31-01 AT MAE ON N/R N01147.SDR 04FDEA03167Roller · wornRIGHT WING INBOARD FLAP UPPER LOAD ROLLER HAS CHROME WORN AWAY ON BEARING SURFACE OF ROLLER. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK FORWARD UPPER LOAD ROLLER IAW FEDEX EA 8-5750-81513, WING - INBOARD ROLLER TORQUE REQUIREMENT - CLARIFICATISDR CA041102003Carriage · cracked(CAN) DURING COMPONENT REPLACEMENT AT HEAVY CHECK, A TYPICAL CRACK WAS DETECTED AT THE SPINDLE JOURNAL FORWARD END ON FLAP CARRIAGE NR 7.SDR ASAA0480572Vane · delaminatedC-CHECK - RT IB FLAP HAS DAMAGED OB VANE DELAMINATED. INSTALLED REPAIR FILLER AND DOUBLER. (K)SDR ASAA0480571Vane · damagedC-CHECK - RT IB FLAP HAS DAMAGED OB VANE. INSTALLED REPAIR FILLER AND DOUBLER.(K)SDR QXEA200400790Skin · chafedPDX - RIGHT HAND OUTBOARD FLAP HAS A SIX FOOT LONG BY 2 INCH WIDE CHAFING MARK ON THE UPPER SURFACE STARTING AT THE INBOARD EDGE WHERE THE FLAP SITS BETWEEN 0 AND 5 DEGREES. REPAIRED IAW RD 8/4-57-106, ISS 7.SDR QXEA200400791Skin · chafedPDX - LEFT HAND OUTBOARD FLAP HAS A SIX FOOT LONG BY TWO INCH WIDE CHAFING MARK ON THE UPPER SURFACE STARTING AT THE INBOARD EDGE WHERE THE FLAP SITS BETWEEN 0 AND 5 DEGREES. REPAIRED IAW RD 8/4-57-016, ISS 7.SDR SWAA043379Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING T/E OUTBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED LT FORE FLAP PER MM.SDR 04FDEA03162Roller · wornLEFT WING INBOARD FLAP INBOARD FLAP ROLLERS MOST FORWARD UPPER LARGE ROLLER WORN. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TRACK FORWARD UPPER LARGE ROLLER IAW FEDEX EA 8- 5750-81513, WINGS, INBOARD FLAP, INBOARD ROLLER TORQUE REQUIREMENTS, CLARIFICATIOSDR 04FDEA03161Roller · corrodedLEFT INBOARD FLAP INBOARD FLAP TRACK AREA, LOWER FORWARD LARGE ROLLER CORRODED ON OUTBOARD SIDE. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TRACK LOWER FORWARD LARGE ROLLER IAW FEDEX EA 8-5750-81513. REFERENCE NON-ROUTINE N00604.SDR 04FDEA03160Roller · wornLEFT HAND INBOARD FLAP INBOARD FLAP TRACK AREA, LOWER FORWARD SMALL ROLLER PLATING WORN. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK LOWER FORWARD SMALL ROLLER IAW FEDEX EA 8-5750-8513, WING INBOARD FLAP INBOARD ROLLER TORQUE REQUIREMENT, CLARIFSDR 04FDEA03159Hinge · corrodedLEFT WING INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, FOUND TO BE OUT OF LIMITS, FABRICATED OVERSIZED REPAIR BUSHING, INSTALLED AND HONED BUSHING IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81528, WINGS - LEFT HAND INBOARDSDR QXEA200400803Structure · chafedPDX - LEFT HAND OUTBOARD FLAP HAS A CHAFING MARK 8 INCH LONG AND .500 INCH WIDE WHICH IS THROUGH THE PAINT AND METAL IS EXPOSED AT FLAP STATION 191 TO 227. REPAIRED IAW RD 8/4-57-388 AND HORIZON AIR EA 6-57-256.SDR QXEA200400789Skin · wornPDX - RIGHT HAND INBOARD FLAP HAS A DEEP WEAR MARK ON THE UPPER SURFACE WHERE THE UPPER SHROUD INBOARD RUB BUTTON SITS. REPAIRED IAW HORIZON AIR EA 6-57-252.SDR QXEA200400792Skin · wornPDX - LEFT HAND INBOARD FLAP HAS A DEEP WEAR MARK ON THE UPPER SURFACE WHERE THE UPPER SHROUD INBOARD RUB BUTTON SITS. REPAIRED IAW HORIZON AIR EA 6-57-253.SDR MWEA040212Vane · chafedLEFT WING FIXED VANE BELOW INBOARD FLIGHT SPOILER HAS A LARGE CHAFE. FABRICATED AND INSTALLED DOUBLER.SDR 04FDEA03142Roller · chippedLEFT WING INBOARD FLAP INBOARD TRACK AREA LOWER AFT LARGE ROLLER PLATING WORN ON SIDE OF ROLLER. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK LOWER AFT LARGE ROLLER IAW FEDEX EA 8-5750-81513, WING, INBOARD FLAP, INBOARD ROLLER TORQUE REQUIREMENT,SDR 04FDEA03137Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BUSHING GALLED. MEASURED BORE DIAMETER AT 1.1725, FOUND TO BE BEYOND DAC MD10 CMM 57-52-02 LIMITS OF 1.150. FABRICATED, INSTALL AND FINAL HONE REPAIR BUSHING IAW DAC CMM 57-52-02 AND EA 8-57SDR UPS04843577Fitting · crackedLT WING STA 419 T/E FLAP CANOE SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D, 51-1-8.SDR 04FDEA03122Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, BORE WAS FOUND TO BE OUT OF LIMITS, ETCHED LUG BORE, ROTO PEENED LUG BORE AND CAD PLATED LUG BORE, FABRICATED BUSHING AND CAD PLATED AND INSTALLEDSDR 04FDEA03127Hinge · corrodedRIGHT WING OUTBOARD FLAP, INBOARD SUPPORT, PIVOT ATTACH POINT, INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUSHING, FOUND TO BE OUT OF LIMITS, INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA 8-5750-83939, WING, RIGHT HANDSDR 04FDEA03126Hinge · corrodedRIGHT HAND INBOARD FLAP, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, FOUND TO BE OUT OF LIMITS, FABRICATED OVERSIZE REPAIR BUSHING, INSTALLED AND HONED BUSHING IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81529, WINGS, RIGHT HAND INBOASDR USAA041042Skin · delaminatedPIT - Q1 - UPPER AND LOWER SKIN, 3.5 INCH X 2 INCH AREA, DELAMINATION, LT IB AFT FLAP OB END UPPER AND LOWER SURFACE. REMOVED DISBONDED SKIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP SKIN DOUBLER IAW SRM.SDR SWAA043335Carriage · wornWHEN FLAPS SELECTED TO 5 DEGREES, HALF WAY BETWEEN 2 & 5 DEGREES FELT VIBRATION, AS FLAPS MOVE INTO WHITE BAND OF 5 DEGREES, VIBRATION WORSE. REMOVED AND REPLACED RT INBOARD FORE FLAP INBOARD AND OUTBOARD CARRIAGES, PER MM.SDR SWAA043330Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED RT FORE FLAP PER MM.SDR GTIA040842Skin · damagedDENT ON LT OB FLAP LOWER SIDE, 19 INCH FROM T/E AND 8 INCHES FROM IB END OF T/E WEDGE, DEPTH 0.095 INCH, DIAM 2.0 INCH. REMOVED DAMAGED SKIN, FABRICATED SKIN AND DOUBLER TREATED AND PRIMED, INSTALLED SKIN AND DOUBLER, BONDED SKINS AND PAINTED.
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