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 ASAA0944823Skin · chafedRIGHT O/B FORE FLAP LWD LEADING EDGE SKIN IS CHAFED 6 INCHES FROM I/B END. REPAIRED FORE FLAP.SDR FDEA200903180957Support Fitting · corrodedRT WING INBD FLAP SUPPORT STRUCTURE FOUND FITTING P/N ANB7394-502 WITH GOUGE AND 4 ATTACHMENT HOLES (FOR ANB7118-502 FITTING) WITH CORROSION ON BORES AND ON LUG FACES. REPAIRED AREA IAW EA 8-5340-128544.SDR IPXA09655158Hinge Fitting · crackedINSPECTION TYPE:C LT WING - I/B MAIN FLAP I/B AFT FLAP HINGE FITTING FOUND CRACKED. CRACK 1.25 INCH AND 1.5 INCH LENGTH. LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 SHT 1 TO 5 REV 43. THIS IS CLASSIFIED AS A MAJSDR IPXA09655140Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER TRAILING EDGE MID AREA THE EXISTING REPAIR PATCH (REF SURVEY SEQ 319-W3-03) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.SDR IPXA09655139Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER TRAILING EDGE I/B AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W3-04) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.SDR IPXA09655137Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER T/E MID AREA THE EXISTING REPAIR (REF SURVEY SEQ 319-W3-02) DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9 REV 43.SDR ASAA0944882Skin · damagedRIGHT WING O/B AFT FLAP DAMAGED. REMOVED PREVIOUS REPAIR AREA, FABRICATED, TREATED AND BONDED NEW SKIN AND DOUBLER REPAIR.SDR ASAA0944849Skin · damagedRIGHT O/B AFT FLAP DAMAGED. REMOVED PREVIOUS REPAIR AREA, FABRICATED, TREATED ,BONDED NEW SKIN AND DOUBLER REPAIR.SDR ASAA0944832Skin · delaminatedRT OUTBOARD FLAP UPPER AND LOWER SURFACES WERE DELAMINATED. REMOVED AND REPLACED RT AFT FLAP IAW AMM 27 51 39.SDR ASAA0944777Skin · debondedLEFT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 44 INCHES FROM I/B END AND 5 INCHES FWD OF AFT EDGE. REPAIRED LT IB MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 44 INCHES FROM IB END AND 5 INCHES FWD OF AFT EDGE. PER SRM 51 70 10.SDR ASAA0944776Skin · debondedRIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN HAS DENT WITH DISBOND 50 INCHES FROM O/B END AND 4 INCHES FWD OF AFT EDGE. REPAIRED RIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN 50 INCHES FROM O/B END AND 4 INCHES FWD OF AFT EDGE.SDR ASAA0944775Skin · debondedRIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 30 INCHES FROM O/B END AND 6 INCHES FWD OF AFT EDGE. REPAIRED RIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 30 INCHES FROM O/B END AND 6 INCHES FWD OF AFT EDGE.SDR ASAA0944770Skin · gougedLEFT O/B FORE FLAP CENTER OF LEADING EDGE SKIN IS GOUGED 6 INCHES FROM I/B. LEFT O/B FORE FLAP REPAIRED GOUGE 6 INCHES FROM I/B ON LEADING EDGE.SDR FDEA200903160923Hinge Bracket · corrodedRIGHT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT LUG OUTBOARD BORE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127487, NEW BUSHING INSTALLED AS PER EA 1-5750-127487. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200903160922Hinge · corrodedRIGHT INBOARD FLAP OUTBOARD HINGE (FLAP MOUNTED) PIVOT LUG INBOARD BORE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127487, BUSHING FABRICATED AS PER MD 11 CMM 57-52-03 REVISION 63 AND NEW BUSHING INSTALLED AS PER E.A. NO. 1-5750-127487. REPAIR CLASSIFIED SDR SWAA091737Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT O/B END. REMOVED AND REPLACED AFT FLAP PER MM.SDR USAA2009032090640Flap · delaminatedCLT - Q5 - MAJOR REPAIR - DELAMINATION ON RIGHT OUTBOARD FORE FLAP TRAILING EDGE AT WBL 300R. REPLACED RIGHT OUTBOARD FORE FLAP IAW B737 AMM 27-51-37.SDR FDEA200903130914Rib · crackedLT INBD FLAP RIB 25A HAS APPROX .125 INCH CRACK RIB 25A - RIB 25A. REMOVED THE UPPER SKIN, DAMAGED RIB, TWO CLOSE OUT PANELS, SIX STIFFENERS, TWO RUB STRIPS AND THE T/E FLAP TIP. LOCATED, DRILLED & DEBURRED RIB. INSTALLED ALL PARTS IAW SRM 51-40-21 PG 7 &SDR DLM88090414Vane · damagedLT WING OTBD FLAP VANE AFT INBD CORNER OF SKIN HAD A GOUGE PENETRATING INTO THE INTERNAL DOUBLER. A SRM 51-70-2 PAR 18B HOT BOND REPAIR WAS INSTALLED THAT EXTENDED AROUND THE VANE LEADING EDGE. THIS REPAIR WAS APPROVED BY BOEING.SDR DLM88090412Vane · damagedLT WING OTBD FLAP IB FIXED VANE HAD 2 GOUGES TO THE SKIN AND PENETRATED INTO THE INTERNAL DOUBLER. DAMAGE WAS NEAR XV1=211 AT THE AFT INBOARD CORNER. DAMAGE WAS CLEANED UP AND AN SRM 51-70-2 PARAGRAPH 18B HOT BOND REPAIR WAS INSTALLED. REPAIR WAS PERMANENTSDR ASAA0944782Wedge · chafedRT WING I/B FLAP TRAILING EDGE WEDGE HAS TWO CHAFED AREAS IN PREVIOUS REPAIRS. REMOVED DAMAGED DOUBLERS, PREPPED AREAS, FABRICATED FILLER AND DOUBLER, BONDED REPAIR IAW B737 400 SRM 51 70 10.SDR ASAA0944752Skin · wornRIGHT I/B EXHAUST GATE UPPER SKIN IS WORN BEYOND REPAIRABLE LIMITS. REPLACED RIGHT I/B EXHAUST GATE PER AMM 27 51 05.SDR ASAA0944744Seal · crackedRIGHT I/B MID FLAP SEAL PLATE ADAPTER PLATE ATTACH FASTENERS ARE LOOSE. REMOVED RIGHT I/B MID FLAP SEAL PLATE ADAPTER FOUND TO BE CRACKED, REPLACED WITH NEW PER SRM 51 40 02.SDR CA090320005Attach Fitting · damaged(CAN) DURING DI, NOTICED THAT THE OTBD LT FLAP SEEMED TO RETRACT TOO FAR INTO THE UP POSITION, ONCE INVESTIGATING, FOUND THAT THE INBD ATTACH BRACKETS (WING STATION 140.110) ON THE AIRFRAME SIDE THAT HOLDS THE OB FLAP ON HAD CRACKED. THE FLAP WAS REMOVED TO ASDR SWAA091697Doubler · missingDURING SCHEDULED MV2 CHECK, FOUND LT WING AFT FLAP I/B TRAILING EDGE REPAIR DOUBLER MISSING. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA091688Flap · crackedDURING SCHEDULED 20Y CHECK, FOUND RT WING O/B AFT FLAP CRACKED. REPAIRED AFT FLAP PER SRM.SDR SWAA091682Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA091678Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING I/B AFT FLAP T/E WEDGE SKIN UPPER I/B CORNER DELAMINATED. REPAIRED SKIN PER SRM.SDR ASAA0954697Arm · chafedRIGHT WING T/E PROGRAM ROLLER ARM IS CHAFED BEYOND SRM LIMITS. REMOVED AND REPLACED ROLLER ARM.SDR UIEA201000109Flap Track · damagedEO DOCUMENTS A MAJOR REPAIR. DURING D-CHECK, DAMAGE WAS FOUND TO 1 FASTENER COUNTERSUNK TO A DEEPER PROFILE (0.730"/100 DEGREE) BEYOND OHM REQUIREMENTS OF THE ORIGINAL DESIGN DIMENSION ( 0.645-0.675" /100 DEGREE REF FIG 1) OF NR 8 FLAP TRACK (PN:65B17061-116, SDR SWIA200921913Fairing · wornRIGHT FLAP STAB FAIRING LIMITS. (C CHECK) REPAIRED PER SRM.SDR ASAA0944710Attach Angle · crackedSEAL RIB ATTACH ANGLE O/B OF NR 3 FLAP TRACK FAIRING COMMON TO LOWER T/E COVE PANEL IS CRACKED. REMOVED AND REPLACED ANGLE.SDR SWAA091662Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING I/B AFT FLAP T/E WEDGE LOWER I/B CORNER DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA091659Wedge · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING I/B MIDFLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR FDEA200903110891Skin · chafedLEFT INBOARD FLAP UPPER SURFACE FOUND CHAFED THROUGH ON SKIN AT 9 INCHES OUTBOARD OF INBOARD END. TRIMMED OFF AS PER SRM 57-10-00 FIGURE 39 VOLUME I REVISION 40. REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIGURE 39 VOLUME I REVISSDR ASAA0944706Skin · gougedRIGHT O/B MID FLAP O/B LOWER AFT SKIN PANEL INNER SURFACE AT NR 3 AND NR 4 FLAP TRACKS. RIGHT O/B MID FLAP O/B LOWER AFT SKIN OUT OF LIMITS AT NR 3 AND NR 4 TRACK PER SRM. DAMAGE WAS REMOVED AT NR 3 TRACK 1 INCH DIAMETER .032 DEEP AT NR 4 TRACK 1 INCH DIA .0SDR ASAA0944704Skin · chafedLEFT O/B MID FLAP O/B LOWER AFT PANEL CHAFED ON INNER SURFACE AT NR 3 AND NR 4 FLAP TRACK. LEFT O/B MID FLAP O/B LWR PANEL AT NR 3 AND 4 TRACK DAMAGE OUT OF LIMIT. REMOVED DAMAGE AT NR 3 TRACK 1" X 2", .032 DEEP AT NR 4 TRACK 1 INCH DIAMETER.SDR ASAA0944705Skin · chafedLEFT O/B MID FLAP O/B LOWER AFT PANEL CHAFED ON PREVIOUS REPAIR 14 INCHES I/B OF NR 1 FLAP TRACK. LEFT O/B MID FLAP O/B LOWER AFT PANEL 14.5 INCHES O/B OF NR 1 TRACK CHAFE MEASURES .018 ORIGINAL THICKNESS .064 OUT OF LIMITS. AREA WAS REPAIRED AND REFINISHED.SDR ASAA0944692Skin · chafedRIGHT O/B MID FLAP LWR AFT SKIN UPPER SURFACE IS CHAFED AT NR 3 AFT FLAP TRACK. OUT OF LIMITS. DAMAGE WAS REMOVED 1" X 2" X .032 REPAIRED.SDR ASAA0944691Skin · chafedRIGHT O/B MID FLAP LWR AFT SKIN LWR SURFACE IS CHAFED AT NR 4 AFT FLAP TRACK. OUT OF LIMITS. DAMAGE WAS REMOVED 1" X 1.5" X .032 REPAIRED PER SRM.SDR ASAA0944690Skin · chafedRIGHT O/B MID FLAP LWR AFT SKIN LWR SURFACE IS CHAFED 13 INCHES O/B OF NR 1 AFT TRACK ON DOUBLER. REPAIRED CHAFED AREA.SDR SWAA091598Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA091597Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA091642Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA09856073Flap · misrepairedINSPECTION TYPE:SV SS 718-W3-24, LT WING I/B FLAP STA XCW 64, 1 LAYER DOUBLER MORE THAN 1 GAGE THICKER THAN BASE STRUCTURE. REPAIRED PER TIMCO REO-G12778 REV A, AND UPS EO DC8-5720-33324-A.SDR ASAA0944703Flap Track · corrodedNR 7 FLAP TRACK CORRODED. NR 7 FLAP TRACK REMOVED AND REPLACED WITH SERVICEABLE UNIT.SDR ASAA0944647Flap Track · corrodedNR 7 FLAP TRACK CORRODED. REMOVED AND REPLACED WITH SERVICEABLE UNIT ON DEFECT.SDR SWAA091516Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR ASAA0944644Spar · crackedLEFT I/B MID FLAP REAR SPAR UPPER CHORD IS CRACKED AT FOUR LOCATIONS NEAR I/B AND O/B NUT PLATE. REMOVED AND REPLACED LEFT I/B MID FLAP REAR SPAR UPPER CHORD PER DWG 65 47841 AND SRM 51 40 02.SDR IPXA09854965Doubler · gougedINSPECTION TYPE:B DAMAGE TO RT OUTBOARD FLAP P/N 5642970-506, S/N UP02702, IPC 27-50-02 FIG 1. DAMAGE CONSISTS OF 0.029 INCH DEEP GOUGE ON AN EXISTING REPAIR DOUBLER AT XF213. REPLACED EXISTING REPAIR DOUBLER PER EO DC8-5750-32622.
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