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 QXEA2011121601365Flap Track · wornRT INBD FLAP NR 1 UPPER FLAP TRACK HAS CARBIDE MISSING ON VERTICAL SURFACE. REMOVED DAMAGE IAW RD 8/4-57-1352. MIN REMAINING THICKNESS .179" REF NTM 51-00-02-250-801. CONFIRMED AREA CRACK FREE REF RD 8/4-57-1352. FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-1720SDR QXEA2011121601364Flap Track · wornLEFT NR 4 FLAP TRACK CARBIDE COATING HAS WEAR ON INBD VERTICAL SURFACE. POLISHED CARBIDE COATING IAW RD 8/4-57-1238. MIN REMAINING THICKNESS .044" FOUND TO BE OUT OF LIMITS. FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-1721.SDR SWAA118287AWedge · delaminatedDURING SCHEDULED HC CHECK, FOUND RT WING IB TE FLAP WEDGE DELAMINATED. R&R WEDGE ASSY IAW MM.SDR ASOA20111210012Torque Box · damagedDURING C-CHECK RIB 19 TORQUE BOX III FLAP ROLLER BUSHING HSG DAMAGED OUT OF LIMITS. MX PERFORMED REPLACEMENT OF RIB 19-TORQUE BOX III IAW EC5710-01181, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWIA201128978Flap · chafedLEFT FLAP VANE LEADING EDGE CHAFED. (C-CHECK) REPAIRED PER SRM.SDR SWIA201128933Vane · chafedRIGHT FLAP VANE LEADING EDGE CHAFED AT 120 WS. (C-CHECK) REPAIR PER SRM.SDR MTNA1209110001Flap · damagedDURING FLIGHT 8106 THE FLAP ASYMMETRY INDICATION APPEARED. AFTER LANDING THE CREW FOUND THE FLAP ON THE LEFT SIDE HAD BEEN DAMAGED. THE FLAP TRANSMITTER WAS REPLACED AND CHECKED GOOD. THE FLAP WAS REPAIRED IAW RDO 201200079-1. AFTER THE REPAIR THE AIRCRAFT SDR DALA1168591610Fairing · delaminatedLEFT WING I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-03 PAR. 5A FIG 5.SDR FDEA201112085240Skin · dentedLT INBD MID FLAP L/E AREA HAS DENT AT WBL 95, WS 194. FOUND OUT OF LIMITS IAW SRM 57-50-1, FIG 3, CUT-OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2 & 57-50-2, FIG 3, INSTALLED REPAIR FILLER AND DOUBLER AT LT INBD MID FLAPS L/E SSDR DALA1168551704Fairing · delaminatedRIGHT WING O/B MAIN FLAP L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PAR. 5A(1).SDR DALA1168541704Fairing · delaminatedLEFT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PAR 5A(1).SDR DALA1168520191Skin · dentedRIGHT WING I/B AFT FLAP LWR SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED AS PER B767-300 SRM 57-53-01. REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201 AND 202.SDR CA111208009Skin · damaged(CAN) ON PREFIGHT WALKAROUND, PILOT DISCOVERED THE RT FLAP TOP CENTER SKIN TO BE TORN WHERE THE CONTROL ROD ATTACHES TO THE FLAP BRACKET.SDR FDEA201112075207Fitting · crackedRIGHT WING AFT FLAP, CRACK FOUND IN FITTING, FITTING REPLACED.SDR FDEA201112075198Skin · corrodedRT OTBD MAIN FLAP LOWER SURFACE PANEL INNER SKIN FOUND CORRODED AT FLAP FWD SPAR, 113" FROM WBL 302.0. REPAIR CARRIED OUT IAW EA F-5750-157102. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201112075197Skin · corrodedRIGHT OTBD MAIN FLAP LOWER SURFACE PANEL INNER SKIN FOUND CORRODED AT FLAP FWD SPAR 1" FROM WBL 302.0. REPAIR CARRIED OUT IAW EA F-5750-157102. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201112075191Skin · corrodedRIGHT OTBD MAIN FLAP LOWER SURFACE PANEL INNER SKIN FOUND CORRODED AT FLAP FWD SPAR 83" FROM WBL 302.0. REPAIR CARRIED OUT ON RT OTBD FLAP OWER SURFACE PANEL SKIN IAW EA F-5750-157102. REPAIR IS CLASSIFIED AS MAJOR.SDR TX9Y20111208008Structure · corrodedLT WING T/E INBOARD MID FLAP T/E LOWER CHORD WAS FOUND CORROSION. THREE CORROSION AREAS WERE FOUND ON LEFT T/E INBOARD MID FLAP (P/N:65B02025-35) T/E LOWER CHORD (P/N:65B02098-1) HORIZONTAL FLANGE LOWER SURFACE. THE REPAIR WAS CARRIED OUT PER BOEING MESSAGE SDR COEA2011120708821Fitting · corrodedHEAVY CK COE / LEVEL 2 CORROSION: RT OUTBOARD FLAP O/B HINGE FITTING PICK-UPS (FWD AND AFT) AT RIB 18 ARE CORRODED AND CRACKED (LENGTH 2", WIDTH 2"). REPLACE FWD ATTACH AND FITTINGS WITH OEM PART ON RIGHT O/B FLAP AT RIB 18 O/B HINGE FITTING AT BL 6907.0.SDR DALA1170751705Fairing · delaminatedLEFT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAM. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA AS PER B767-300 SRM 57-53-01 REPAIR 1 AND B767-300 SRM 51-70-05 PAR 5A(1) FIG 5.SDR DALA1170741705Fairing · delaminatedLEFT WING O/B FLAP MID L/E FAIRING O/B AREA FOUND DELAM. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA AS PER B767-300 SRM 57-53-01 REPAIR 1 AND B767-300 SRM 51-70-05 PAR 5 A(1).SDR DALA1170731705Wedge · delaminatedLEFT WING O/B FLAP AFT WEDGE LWR SURFACE AT NR 1 FAIRING I/B AREA FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINTED AREA AS PER B767-300 SRM 57-53-01 REPAIR 1 AND B767-300 SRM 51-70-07.SDR QXEA2011122001414Flap Track · wornLEFT NR 1 FLAP TRACK WORN. BLENDED DAMAGE IAW RD 8/4-57-1352. PERFORMED ULTRASONIC THICKNESS MEASUREMENTS. MAX WEAR NOTED .008". PRIMED TRACK IAW SRM 51-25-10-02-01. TOPCOATED TRACK IAW RD 8/4-57-1716. PERFORMED ECI ON BLENDED AREAS, NO CRACK FOUND AT THSDR WX0A071019Skin · dentedLEFT WING INBOARD FLAP LOWER SURFACE DENTED, STA XW91 23 INCHES FROM T/E (INBD NR 34) MEASURES DIA 1.5" X .062 DEEP. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, FILLED, DOUBLER AND INSTALLED IAW MD80 SRM 57-01, FIG 5.SDR UALA2011120606691Structure · damagedLEFT FLAP INBD TRAILING EDGE HAS DAMAGE. CUT OUT DAMAGE, POTTED IN REPLACEMENT CORE. REPAIRED WITH 250 DEGREE OVERLAY REPAIRS PER SRM.SDR USAA2011122800017Flap · debondedC2 CHECK - DISBONDED RIGHT WING OUTBOARD FLAP TRAILING EDGE BETWEEN WS 309.125 TO WS 311.625, 64 INCHES FROM OUTBOARD EDGE. REPAIRED RIGHT WING OUTBOARD FLAP TRAILING EDGE BETWEEN WS 309.125 TO WS 311.625, 64 INCHES FROM OUTBOARD EDGE IAW B767 SRM 51-70-05-0GSDR FDEA201112045140Skin · dentedLEFT INBD T/E MIDFLAP TOP AREA INBD SIDE HAS THREE DENTS. FOUND OUT OF LIMITS IAW SRM 57-50-1, FIG 3, CUT-OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2 & 57-50-2, FIG 3, INSTALLED REPAIR FILLER AND DOUBLER AT LT INBD MID FLAPS L/ESDR FDEA201112045139Skin · dentedLEFT WING OTBD MIDFLAP HAS A DENT ON LOWER SURFACE OF L/E, 15" FROM OTBD END OF FLAP. CUTOUT DAMAGED AREA IAW SRM 57-50-4, FIG 2. FABRICATED DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2. INSTALLED DOUBLER, FILLER AND FASTENERS IAW SRM 57-50-4, FIG 2 & EA 7-575SDR DALA1167281704Skin Panel · delaminatedRT WING O/B FLAP UPPER PNL 666MT LWR SURFACE FOUND DELAM METAL. HOT BOND REPAIR PERFORMED PER B767-300 SRM 57-53-01, REPAIR 1 FIG 201 AND SRM 51-70-10, REPAIR 4 FIG 202.SDR A6WA201240144Guide · chafedLT OTBD ROLLER GUIDE CHAFED. BLENDED LT OTBD FLAP ROLLER GUIDE, REMAINING MATERIAL IS WITHIN SERVICEABLE LIMITS IAW REO 601R57-51-143, TOTAL AMOUNT REMOVED 0.008, MAX ALLOWED 0.005.SDR SWAA118681Flap · delaminatedDURING SCHEDULED 20Y CHECK, FOUND DELAMINATION ON I/B SIDE OF O/B AFT FLAP. REMOVED AND REPLACED FLAP PER MM.SDR SWIA201128825Rib · dentedRIGHT WING INBOARD FLAP HAS A DENT ON THE BOTTOM TRAILING EDGE. (SERVICE) FOUND DAMAGE TO THE FLAP RIBS BETWEEN FLS 30.00 AND FLS 42.00. REPLACED THE DAMAGED RIBS PER SRM.SDR FDEA201112025116Skin · dentedRT WING T/E OTBD FLAP UPPER SURFACE DENTED. REPAIRED IAW SRM 57-53-12 FIG 210. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201112015099Skin · gougedRIGHT WING OTBD FOREFLAP L/E SKIN GOUGED IN 2 PLACES ABOVE NR 7 FLAP CARRIAGE. REPAIRED IAW SRM 57-50-2, FIG 4 & SRM 57-50-4, FIG 1 & EA 7-5750-143963.SDR FDEA201112015129Skin · delaminatedLEFT WING INBD FLAP UPPER SURFACE AT MAIN FLAP STA 200 HAS AN AREA WITH SIGNS OF DELAMINATION. REPAIRED IAW SRM 51-70-10, REPAIR NR 4. REF EA F-5750-147773. MAJOR REPAIR.SDR FDEA201112015104Skin · misrepairedRT WING CENTER FLAP LOWER MAIN SKIN BETWEEN STRINGERS 1.1 TO 2.4 AT RIBS 17 AND 19, MISINSTALLED. REPAIRED SKIN PER AND COMPLIED WITH EA 6-5750-145694.SDR DALA1166411607Flap · dentedLT WING I/B MAIN FLAP LWR MID AREA IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.SDR SWIA201131336Vane · chafedLEFT INBOARD FLAP VANE IS CHAFED OUTBOARD LEADING EDGE. (C-CHECK) REPAIRED PER REO.SDR SWIA201131335Vane · chafedLEFT INBOARD FLAP VANE IS CHAFED AT INBOARD LEADING EDGE. (C-CHECK) REPAIRED PER REO.SDR SWIA201131334Vane · chafedLEFT INBOARD FLAP VANE IS CHAFED AT CENTER LEADING EDGE. (C-CHECK) REPAIRED PER REO.SDR FDEA201111305095Skin · damagedLEFT TE FLAP LE HAS LARGE CREASED AREA TOP SIDE. REMOVED DAMAGE AREA SKIN AND CORE ON LT INBD T/E L/E, FABRICATED, HOT BONDED CORE AND DOUBLER REPAIRS, CLEANED, SEALED, & FINISHED IAW SRM 51-40-20 & EA 7-5750-143964.SDR SIMA201133603Flap · damagedDURING MAINTENANCE BASE INSPECTION DID PERMANENT REPAIR OF LEFT OUTBOARD FLAP BLIND FASTENER (EO CR-5700-107). THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT HAND OUTBOARD FLAP AS PER EO CR-57MR-107. THE AIRCRAFT WAS RETURNED TO SERIVCE.SDR SWAA118260Flap · puncturedDURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP IAW SRM.SDR A6WA201240045Hinge Fitting · chafedRT INBD FLAP INBD HINGE BOX TOP INBD LUG CHAFED. REPAIRED RT INBD FLAP INBD HINGE BOX LUG IAW REO 601R-57-21-1554.SDR FDEA201111295069Structure · crackedRT WING INBD MID FLAP T/E CHORD CRACKED AT INBD FLAP CONTROL DRUM, WBL 100. REMOVED MID FLAP T/E CHORD IAW SRM 51-30-2. LOCATED AND DRILLED NEW CHORD IAW SRM 57-50-2, FIG 5 AND INSTALLED NEW CHORD SECTION, USED PREVIOUS REPAIR IAW SRM 57-50-2, FIG 5 & EA 7-57SDR FDEA201111295076Skin · misrepairedRT WING CENTER FLAP T/E SKIN LOWER SURFACE BETWEEN RIBS 17 AND 19 LOCATED 3.5" FWD OF AFT EDGE IS INSTALLED INCORRECTLY. REPAIRED IAW SRM 57-50-00, FIG 205 PAGES 217 TO 220 AND COMPLIED WITH EA 6-5750-156074, WC 57504134, SEQ 1242.SDR SWAA118188Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT I/B LOWER CORNER. REMOVED AND REPLACED AFT FLAP IAW MM.SDR IPXA1M70470Skin · dentedRT WING INBD FLAP T/E UPPER SKIN DENT BETWEEN X1FH 159.3 - X1FH 153.3 6" FROM T/E OF WEDGE. REPAIRED IAW EO MD11-5750-45198-A.SDR IPXA1M70469Skin · dentedRT WING INBD FLAP T/E UPPER SKIN DENT BETWEEN X1FH 159.3 - X1FH153.3 2 3.0" FROM T/E OF WEDGE. REPAIRED IAW EO MD11-5750-44592-C.SDR SWIA201131124Vane · chafedRIGHT OUTBOARD FLAP VANE ON INBOARD FLAP CHAFED. (C-CHECK) REPAIRED IN REFERENCE TO CRJ200 REO.
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