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 A6WA200740556Skin · dentedLEFT INBOARD FLAP UPPER SKIN DENTED 15 INCHES FROM INBOARD EDGE, 7 INCHES FROM TRAILING EDGE APPROX 1.25 INCH LONG BY 1 INCH WIDE BY .022 INCH DEEP. MAINTENANCE REPAIRED LT INBOARD FLAP UPPER SKIN USING NON-FLUSH REPAIR IAW CRJ 200 SRM 57-52-00 REPAIR NR 03. SDR 2007UALA04133Bearing · migratedA-C HAD A ROUGH BUFFET WITH FLAPS FULL. ALL OTHER CONFIGURATIONS NORMAL. PROBLEM RECURRED ON FLT 0532-15OCT. INSPECTED NR 1 FLAP CARRIAGE SPHERICAL BEARING FOUND SLIGHTLY MIGRATED BUT AIRWORTHY. OPENED A REPETITIVE INSPECTION PROGRAM TO TRACK THE MIGRATIONSDR 07FDEA04499Rib · crackedRT INBOARD FLAP RIB 25 FOUND CRACKED REMOVED SKIN AND STRINGERS. REMOVED DAMAGED RIB 25. INSTALLED NEW RIB 25 AND RE-INSTALLED SKIN AND STRINGERS. SEALED AND PAINTED.SDR ASAA0782085Doubler · chafedRIGHTHAND WING OUTBOARD FLAP INBOARD FIXED VANE L/E DOUBLER IS CHAFED. REPLACED EXISTING DOUBLER PER SRM 51-70-2.SDR ASAA0782084Vane · gougedLEFTHAND WING OUTBOARD FLAP INBOARD VANE L/E DOUBLER REPAIR IS GOUGED. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70-2.SDR BSAASDR0725Skin · tornRIGHT FLAP HUMP MISSING LARGE SECTION OF SHEET METAL. FLAP WAS REMOVED AND REPLACED.SDR USAA920071127Skin · delaminatedCLT - MAJOR REPAIR - C20 CHECK, RIGHT WING AILERON UPPER LEADING EDGE HAS EXPOSED CARBON FIBLER. REPLACED RIGHT WING AILERON IAW TASK CARD R3M27015.SDR UPS07M51048Structure · corrodedINSPECTION TYPE:C RIGHT WING: DURING O/B FLAP I/B FWD HINGE PIVOT BEARING REPLACEMENT FOUND PIVOT BORE CORRODED AS MARKED. RIGHT O/B FLAP I/B FWD HINGE REMOVED PER AMM 57-53-01 R.50. RIGHT FWD O/B FLAP I/B HINGE PIVOT BORE CORROSION REMOVED & FOUND EXCEED LSDR SWAA074931Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA04479Skin · dentedLEFT WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE FOUND DENT. 10-12-07 REPAIR CARRIED OUT AT LEFT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR TRAX200701480Bracket · brokenON RIGHT WING O/B FLAP ARM AT RIB 13, 1 OMEGA BRACKET BROKEN OFF TO BE FABRICATED.SDR UIEA200700429Skin · nickedLEFT WING T/E FLAP INBOARD AFT FLAP LOWER SURFACE HAS VARIOUS NICKS AND SCRATCHES. INTERIM REPAIR CARRIED OUT IAW SRM 57-53-01, AND XEO 57-092607.SDR UIEA200700428Skin · nickedRIGHT INBOARD T/E FLAP AFT FLAP LOWER SURFACE HAS VARIOUS NICKS. INTERIM REPAIR CARRIED OUT IAW SRM 57-53-01, AND XEO 57-092607.SDR TRAX200701463Bracket · brokenLT I/B FLAP, O/B FLAP ARM (3) OMEGA BRACKETS BROKEN.SDR 07FDEA04460Skin · misrepairedFOUND OLD POCKET REPAIRS AT RIB 21 INBOARD FLAP LT NOT CONFORM TO SRM. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB 57-2055.SDR 07FDEA04452Rib · damagedFOUND OLD REPAIRS ON INBOARD FLAP RIB 21 (POCKET REPAIRS) NOT CONFORM TO SRM REPAIR PERFORMED BY REPLACEMENT OF END RIB 21 IAW SRM 57-2055.SDR 07FDEA04448Skin · damagedRT INNER FLAP WITH SEVERAL DAMAGES, LIMITED TO 5 FLIGHTS IAW RAS/DABRE/7002673/2003. REPAIR PERFORMED IN WORKSHOP AND RELEASED IAW FAA FORM 8130-3 NR 05/1145.SDR FDEA200710014430Skin · looseDURING INSPECTION ON LT WING OTBD FLAP UPPER SKIN FOUND 200 LOOSE FASTENERS. REPAIRED AREA IAW SRM 51-35-01 PAR 1-5 VOL II.SDR FDEA200710014429Skin · looseDURING INSPECTION ON LT WING OTBD FLAP LWR SKIN FOUND 100 LOOSE FASTENERS. REPAIRED AREA IAW SRM 51-35-01 PAR 1-5 VOL II.SDR 2007UALA03964Skin · delaminatedLEFT MID FLAP DELAM AND DAMAGE. LEADING EDGE INBOARD, EXTENDING OUT APPROX 5 INCHES. SUSPECT MOISTURE CONTAMINATION. REPLACED THE LT OUTBOARD FLAP PER MM-27-51-04. AC OK FOR SERVICE.SDR 2007UALA03963Structure · damagedRIGHT OUTBOARD AFT FLAP HAS 3 INCH DIA HOLE, BOTTOM AT APPROX 4 FT OUT FROM INBOARDD EDGE AND 7 INCHES UP FROM T/E. REPAIRED IAW SRM 51-70-02. AC OK FOR SERVICE.SDR SWAA074890Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA04430Skin · looseDURING INSPECTION ON LT WING OUTBD FLAP UPPER SKIN FOUND 200 LOOSE FASTENERS.SDR 07FDEA04429Skin · looseDURING INSPECTION ON LT WING OUTBD FLAP LWR SKIN FOUND 100 LOOSE FASTENERS.SDR 07FDEA04425Skin · looseDURING INSPECTION ON RT WING OUTBD FLAP LWR SKIN FOUND 50 LOOSE FASTENERS.SDR SWAA074869Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER BOEING SB.SDR UIEA200700419Fairing · delaminatedRT WING NR 5 FLAP TRACK FORWARD FIXED FAIRING AT WBL 235.20, OUTBOARD SIDE HAS AN AREA 12.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION AND CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 6, SHEETS 1 THRU 4 AND SRM 51-40-12. ALSO, REFERESDR USAA920070885Support Beam · crackedMCN - MAJOR REPAIR - NR 5979695 - RIGHT WING INBOARD FLAP, INBOARD FLAP BELLCRANK SUPPORT BEAM CRACKED, WS 152. REMOVED AND REPLACED RIGHT WING INBOARD FLAP, INBOARD FLAP BELLCRANK SUPPORT BEAM FITTING, WS 152 - RIG AND OPS CHECK GOOD IAW BOEING SOPM 20-50-01SDR 1218344112107Beam · corrodedCORROSION ON LEFT WING FLAP BEAM AT RIB 8, FOUND TO BE BEYOND LIMITS. LEFT WING FLAP BEAM RIB 8 REPLACED.SDR 07FDEA04353Skin · failedEXISTING EXTERNAL REPAIR DOUBLER ON NOSE SKIN OF OUTBOARD RT FLAP, RIB 10.5 (PANAM EA X3157J518). PERMANENT REPAIR WAS CARRIED OUT ON 25-APR-1994 BY REPLACING THE INSTALLED DOUBLER WITH A 1,8MM THICK ONE AND THE EXISTING FASTENERS WITH BLIND RIVETS CR35SDR 1218342121707Fitting · corrodedRIGHT INBOARD FLAP, FLAP ARM AND FLAP BEAM CORRODED AT FLAP RIB 5. RIGHT INBOARD FLAP BEAM, FLAP, FLAP ARM REPLACED AT RIB 5.SDR SWAA074850Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA074847Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR 07FDEA04344Skin · failedFOUND OLD DOUBLER REPAIR ON LOWER PANEL, CENTER BOX OF INBOARD FLAP RT, RIB 9-11, NOT IAW SRM 57-52-12/FIG 205, DOUBLER EDGES, LENGTH OF DOUBLER SHEET NOT ALLOWED. REPAIR RENEWED AS PER SRM 57-52-12/FIG 205, RIB 9. REPAIRED AS PER SRM 51-40-51/FIG 202, ALL ISDR 07FDEA04343Skin · failedFOUND OLD REPAIR ON CLOSING RIB 21, INNER FLAP RT FINAL REPAIR ON FLAP BY REPLACEMENT OF END RIB 21 IAW SB A310-57-2055/PARA 2 F.SDR MASA200700742Fitting · unknownREPAIR TO O/B FLAP LUG FITTING WS 178 AND 264.SDR 07FDEA04319Rib · crackedLT RIB 25 AND RT RIB 25 FOUND CRACKED IN "B" CHECK. REPLACED RIB 25 LEFT AND RIGHT INBOARD FLAPS.SDR UPS07850855Attach Angle · crackedINSPECTION TYPE:C1 RIGHT WING AT STA 3 FITTING ATTACH L-ANGLE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR L-ANGLE AT RIGHT WING FLAP STA 3 IAW DWG 5643117, AND SRM 51-03-00.SDR 07FDEA04299Skin · crackedFOUND AT LT INNER FLAP LOWER SKIN CRACKED (4MM) AND HOLES DAMAGED REPAIR PERFORMED BY REMOVAL OF CRACKS AND OVERSIZING THE DAMAGED HOLES IAW EA 6-5752-112505 AND RAS/FOK/024/2007 ISS A.SDR NWAA073416301Spar · gougedDURING "M" CHECK, FOUND GOUGE ON AFT WEB OF THE INBOARD FORE FLAP FRONT SPAR JUST OUTBOARD OF WBL 134.8. REPAIRED PER EA 63-210697 SECTION I. SECTION II REQUIRES INSPECTION OF REPAIR AT "L" CHECK INTERVALS. SECTION III CALLS OUT PERMANENT REPAIR NEXT "H" CHSDR UIEA200700387Skin · delaminatedRIGHT WING OUTBOARD FORE FLAP HAS DELAMINATION FROM WBL 804-WBL 817. REPAIRED RIGHT OUTBOARD FOREFLAP LEADING EDGE AT WBL 804 TO WBL 817 IAW SRM 51-70-07 AND ATLAS XEO 57-091507.SDR 07FDEA04272Skin · chafedLT OUTER FLAP CHAFING DAMAGE AT TOP SKIN AT RIB 4 AND 15A AFT OF T/E SKIN SPLICE. REPAIR PERFORMED BY SMOOTHLY BLEND THE DAMAGED AREAS WITHOUT INCREASING DEPTH IAW TD FOK/154/2005 ISSUE A, APPROVED BY EA 6-5753-92138 AND RAS/FOK/154/2005 ISSUE A.SDR 07FDEA04271Skin · chafedLT AND RT CENTER FLAP CHAFING DAMAGE AT TOP SKIN AT RIB 15 AND 23 AFT OF T/E SKIN SPLICE. REPAIR PERFORMED BY SMOOTHLY BLEND THE DAMAGED AREAS WITHOUT INCREASING DEPTH IAW TD FOK/153/2005 ISSUE A, APPROVED BY EA 6-5753-92137 AND RAS/FOK/153/2005 ISSUE A.SDR SWAA074772Skin · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR 07FDEA04224Skin · dentedRT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA04221Skin · dentedLT WING INBOARD FLAP LOWER SEGMENT FOUND WITH SEVERAL DENTS. 10-05-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 2007UALA03937Carriage · damagedLEFT OUTBOARD FOREFLAP OUTBOARD SEQUENCE CARRIAGE OUTBOARD SLIDER IS DAMAGED AND ATTACH BOLTS INSIDE FAIRING. REPLACED LEFT OUTBOARD FORE FLAP OUTBOARD SLIDER.SDR SWAA074749Torque Tube · wornDURING SCHEDULED A1 CHECK, FOUND LEFT WING NR 4 T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA074750Torque Tube · wornDURING SCHEDULED A1 CHECK, FOUND RIGHT WING NR 5 T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA074743Repair · missingRIGHT WING INBOARD FORE FLAP PREVIOUS REPAIR PATCH MISSING. REMOVED AND REPLACED FORE FLAP PER MM.
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