JASC 5753
Service difficulty reports · 31,513
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 DALA1217433148Trunnion · damagedLEFT INBOARD FLAP TRUNNION DAMAGED. AREA WORN APPROXIMATE .250 DEEP. REMOVED LEFT INBOARD FLAP INBOARD TRUNNION IAW A319/320 CMM 57-52-21 (903393). REPLACED LEFT INBOARD FLAP TRUNNION IAW A319/320 CMM 57-52-21 AND PER PRI501285-14 REV 1. INSTALLED INBOARDSDR GR4D20120321020Flap Track · corrodedFLAP TRACK CORRODED, ULTRA SONIC NDT INSPECTION COMPLIED WITH. AFTER ENGINEERING EVALUATION, REMAINING THICKNESS WAS UNACCEPTABLE. REF B/P SE05811901, REV D. REF CMP GIV MESSAGE 3575111 FOR INSPECTION.SDR UALA2012031901753Flap · damagedL/E FLAP DAMAGED BY RUNAWAY STAND IN HEAVY WINDS. REPLACED NR 10 L/E FLAP IPC 27-81-02- 010 ITEM 10.SDR FDEA201203170988Hinge Fitting · corrodedRIGHT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET LOWER INBD STUD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.592", FINAL HOLE DIAMETER 0.611", MAXIMUM ALLOWABLE DIAMETER 0.584". REPAIRED IAW EA 1-57SDR FDEA201203170986Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD FWD HINGE BRACKET SIDE LOAD FITTING ATTACH SURFACE FOUND CORRODED. AREA REWORKED IAW CMM 57-44-09, REV 72. EXISTING THICKNESS UPPER 0.406", LOWER 0.406", REMAINING THICKNESS UPPER 0.400", LOWER 0.400". REPAIRED IAW EA 1-5750-157158 SDR SWAA2012032902657Skin · delaminatedLT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2012032602590Skin · puncturedRIGHT WING I/B FOR FLAP LOWER SURFACE PUNCTURED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2012032602549Flap · delaminatedLEFT WING O/B AFT FLAP DELAMINATED AT LOWER I/B SIDE. REMOVED AND REPLACED AFT FLAP IAW SRM & AMM.SDR IPXA12B72500Fairing · puncturedINSPECTION TYPE: C, RT WING INBD AFT FLAP L/E FAIRING PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 60.SDR IPXA2672455Wedge · chafedINSPECTION TYPE:C, LT WING INBD T/E AFT FLAP CHAFED ON UPPER SKIN AT IFS 105.750. APPROX LT X W=1" X 1.25" ON UPPER SKIN CUT OUT THE CHAFED SIZE L X W=1" X 1.25". PERFORM THE REPAIR IAW REV: 52, SRM 57-53-01, REPAIR 1, FIG 201, SHEET 4 OF 6 AND 51-70-10 REPASDR IPXA2672453Wedge · chafedINSPECTION TYPE:C, RT WING INBD T/E AFT FLAP CHAFED ON UPPER SKIN AT IFS 105.750 APPROX L X W=1.1" X 1.24" ON UPPER SKIN CUT OUT THE CHAFED SIZE L X W=1.1" X 1.24". PERFORM THE REPAIR IAW REV:52, SRM 57-53-01. REPAIR 1, FIG 201 SHEET 4 OF 6 AND 51-70-10, REPSDR CA120507018Cable · frayed(CAN) INSPECTED FLAP CABLES AND FOUND FLAP CABLES 1460100-7 AND 1460100-8. FRAYED AT LOCATIONS SHOWN IN ALERT. CABLES R & R WITH NEW.SDR FDEA201203140931Vane · corrodedRT WING OTBD FLAP VANE FITTING, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02, FIG 201, REV 48. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1-5750-150450. PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201203140930Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATION. R & R IAW AMM 27-50-22-4, REV 72.0. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY IAW AMM 27-50-22-5, REV 72.0. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 114.SDR FDEA201203140929Vane · delaminatedRT WING INBD FLAP VANE UPPER SURFACE FOUND DELAMINATION. R & R IAW AMM 27-50-22 REVISION 72.0. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY IAW AMM 27-50-22-5, REV 72.0. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 114.SDR SWAA2012031602249Flap · delaminatedRT WING AFT T/E FLAP DELAMINATED JUST AFT AND INBOARD OF THE NR 2 AFT FLAP TRACK. REPAIRED FLAP PER SRM.SDR SWAA2012031402196Flap · delaminatedLT WING TRAILING EDGE O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR FDEA201203130912Fitting · corrodedRIGHT WING OTBD FLAP VANE FITTING F ECCENTRIC HOLE FOUND CORRODED. FOUND EXCEEDED LIMITS IAW SRM 57-50-02 FIG 201, REV 48 EXISTING HOLE:0.851"(LENGTH), 0.557"(WIDTH). FINAL HOLE 0.944"(LENGTH), 0.660"(WIDTH). MAXIMUM HOLE 0.940"(LENGTH), 0.670"(WIDTH).REPAIR SDR FDEA201203130911Fitting · corrodedLEFT WING OTBD FLAP VANE FITTING B ECCENTRIC HOLE FOUND CORRODED. FOUND EXCEEDED LIMITS IAW SRM 57-50-02, FIG 201, REV 48 EXISTING HOLE:0.873"(LENGTH), 0.623"(WIDTH). FINAL REWORK HOLE 0.930"(LENGTH), 0.706"(WIDTH). MAXIMUM REWORK HOLE 0.940"(LENGTH), 0.640"SDR A6WA201240335Vane · chafedLEFT INBD FLAP VANE L/E CHAFED IN 3 AREAS (FOUND INBD FWD RIG TO HAVE DOUBLER DRILLED HOLES) R & R LT INBD FLAP VANE INBD L/E PN 601R14303-53S & END RIB 601R14304-13 IAW SRM 51-40-11 AND 51-42-13.SDR SWAA2012040302801Skin · delaminatedLT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM AND AMM.SDR SWAA2012031302143Flap · delaminatedRT WING AFT O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR FDEA201203120893Hinge Fitting · damagedLT WING (FLAP SIDE) INBD FLAP OTBD HINGE INBD PIVOT HOLE FOUND STEP HOLE. MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 . EXISTING HOLE DIA 1.190", /1.253" , MAXIMUM HOLE DIA 1.220" BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-150446, PART 1 SDR FDEA201203120892Bushing · wornLT WING (FLAP SIDE) INBD FLAP OTBD HINGE OTBD PIVOT HOLE BUSHING WORN. REMOVED IAW CMM 20-20-07, REV 72 EXISTING HOLE DIA 1.283", MAX ALLOWABLE HOLE DIA 1.220" HOLE MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 . BUSHING FABRICATED AND INSTALLEDSDR FDEA201203120890Bushing · wornRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE INBD PIVOT HOLE BUSHING WORN. BUSHING REPAIRED IAW EA 1-5750-160001, PART 1. EXISTING HOLE DIA 1.283", MAX HOLE DIA 1.220", NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-160001 PART 1, STEP 4 AND 5. REPAIR CLSDR FDEA201203120889Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP OTBD HINGE OTBD PIVOT HOLE FOUND STEP HOLE. REPAIRED IAW EA 1-5750-160001, PART 1. EXISTING HOLE DIA.1.282" /1.192", MAX ALLOWABLE HOLE DIA 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-160001 PART 1, STEP 4 ANSDR SWAA2012031302136Flap · delaminatedRT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.SDR SWAA2012031202118Skin · delaminatedRT WING AFT FLAP O/B TRAILING EDGE I/B AND UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER MM.SDR A6WA201240420Vane · chafedLEFT INBD FLAP VANE CHAFED ON UPPER INBD T/E. REPAIR LT INBD FLAP VANE ON UPPER INBD T/E IAW SRM 51-12-00 AND SRM 57-52-00.SDR USAA2012031300015Skin · damagedC4 CHECK - SMALL 1 INCH SPLIT IN RIGHT INBOARD AFT FLAP ON OUTBOARD END AT WS 258.50, WBL 740. REPAIRED RIGHT INBOARD AFT FLAP SKIN IAW B757 SRM 51-70-17.SDR CA120309005Bearing · worn(CAN) DISCOVERED FLEETWIDE PROBLEM WITH THE OTBD FLAPS, INBD AFT HINGE, OTBD RIB BRACKET. THE FLAP ROLLER BEARING, PN BC56985, CAN WEAR, ALLOWING THE BEARING FLANGE TO CONTACT AND WEAR THE FLAP RIB, CALLED A BRACKET, PN 35-165050-30 AND -31. ALL 5 COMPANY ACSDR DALA1214471503Skin · delaminatedRT WING O/B TRAILING EDGE FLAP LWR SURFACE FOUND DELAMINATED AT I/B LWR SIDE. REPAIRED IAW B767-300 SRM 57-53-01 REPAIR 1 TABLE II AND SRM 51-70-01 PARA 5A FIG 9.SDR CA120307004Bearing · rough(CAN) BEARING ROUGH. CENTER PORTION MIGRATED TO OR WAS MFG BELOW THE SURFACE OF FLANGE CAUSING DAMAGE TO ADJACENT BRACKET. DISCOVERED WHEN FLAP WAS REMOVED FOR UNRELATED REASON.SDR FDEA201203070796Attach Fitting · crackedRIGHT WING T/E OTBD FLAP L/E STOP BOLT ATTACHMENT FITTING FOUND CRACKED. ATTACH FITTING REMOVED AND REPLACED AS PER EA 1-5750-160011.SDR FDEA201203070795Attach Fitting · crackedLEFT WING T/E OTBD FLAP L/E STOP BOLT ATTACHMENT FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER EA 1-5750-160010. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 114.SDR AALA20120314010Skin · gougedRIGHT WING INBOARD MID FLAP BOTTOM SIDE HAS GOUGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07 AND AMM 51-20-00-0.SDR UALA2012030801531Screw · missingTWO ADJACENT SCREWS MISSING LEFT WING INBD MOST FLAP ASS'Y CANOE OTBD SIDE TOP AFT. REPLACED MISSING SCREWS ON INBD FLAP INBD FLAP CANOE 2EA.SDR FDEA201203070865Skin · delaminatedLEFT WING FLAP DELAMINATED T/E BETWEEN NR 1 AND NR 2 CANOE APPROX 10" X 10" AREA . REMOVED LT OTBD T/E FLAP REF MM 27-51-21-4. T/E FLAP SYS MAINT PRACTICES COMPLIED WITH IAW MM 27-51-00-2. REMOVAL/INSTALLATION COMPLIED WITH IAW MM 27-51-21-4 AND OTBD T/E FLASDR IPXA2672231Wedge · damagedINSPECTION TYPE: C, LEFT WING OTBD T/E FLAP HAS PUNCTURE (2"X1")ON L/E. LOCATED 2' OTBD OF INBD EDGE ON THE L/E. REMOVE THE EXISTING INTERIM REPAIR FOR SIZE L X W=5.1"X2.5". PERFORM THE REPAIR IAW REV:52,767-300F, SRM 57-53-01, REPAIR 1, TABLE I AND SRM 51-SDR IPXA2672230Skin · dentedINSPECTION TYPE: C, DENTED SKIN, LT WING OTBD FLAP LOWER SKIN DENTS AT OTEF STA 250 AND OTEF STA 263.5. DENT WITH DELAMINATION DIMENSION L X W X D=2.2"X2.1"X0.020" AT OTEF STA 250 AND THE OTHER DENT WITH DELAMINATION DIMENSION L X W X D=2.0"X1.54"X0.020" AT OSDR DALA1213711503Spar · corrodedRT WING I/B FLAP STA 124 REAR SPAR LOWER CHORD CORRODED. PERMANENT REPAIR PERFORMED IAW ERA 496155-14 REV 0.SDR AALA20120307024Skin · dentedRIGHT WING TRAILING EDGE INBOARD FLAP LOWER TRAILING EDGE INNER SKIN DENTED. INSTALLED DOUBLER REPAIR PER SRM 57-53-01 AND SRM 51-70-10.SDR A6WA201240413Rib · damagedLEFT INBD FLAP HAS MISDRILLED HOLES UNDER INBD SEAL PN 601R14016-31 RIB ASSY. R & R LT INBD RIB ASSY PN 601R14016-31.SDR A6WA201240427Rib · damagedLEFT INBD FLAP HAS MISDRILLED HOLES UNDER INBD SEAL PN 601R14016-31 RIB ASSY. R & R LT INBD RIB ASSY PN 601R14016-31.SDR IPXA2B72324Skin · damagedINSPECTION TYPE: C, LEFT WING OTBD AFT FLAP LWR SURFACE FOUND DAMAGED HOLE METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 2, REV 60.SDR IPXA12672177Fairing · delaminatedINSPECTION TYPE: 9C, RIGHT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1), FIG 5, REV 52.SDR VNAA2012030900005Fairing · damagedDURING PREFLIGHT INSPECTION, CREW REPORTED DAMAGE TO RIGHT WING ON INBOARD FAIRING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO RIGHT INBOARD FLAP INBOARD HINGE FAIRING TO BE FROM LIGHTNING STRIKE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REPAIRED RISDR DALA1213750180Flap · delaminatedRT WING I/B MAIN FLAP LEADING EDGE O/B FAIRING FOUND DELAMINATED. REPAIR PERFORMED IAW B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.SDR DALA1213740180Flap · delaminatedLT WING I/B MAIN FLAP LEADING EDGE O/B FAIRING FOUND DELAMINATED. REPAIR PERFORMED IAW B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.SDR DALA1213701503Flap · dentedRT WING O/B FLAP LWR SIDE FOUND DENT. REPAIRED IAW B767-300 SRM 57-53-01 REPAIR 1 AND REPAIR INSTRUCTION IAW B767-300 SRM 51-70-10 REPAIR 2 FIG 203.
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