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 ASAA0510123Skin · chafedYXX - FOUND RIGHT INBOARD FORE FLAP CHAFED DAMAGED ON OUTBOARD TOP SURFACE AT WBL 181. RIGHT INBOARD FORE FLAP, OUTBOARD TOP SURFACE AT WBL 181 CHAFED LOCATION REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 4 FIGURE 13. (M)SDR ASAA0510122Skin · dentedYXX - RIGHT INBOARD FORE FLAP DENTED AND DELAMINATED AT OLD REPAIR AT WBL 118. RIGHT INBOARD FORE FLAP AT WBL 118 DENTED AND DELAMINATED LOCATIONS REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 7 FIGURE 16. (M)SDR 05FDEA01524Skin · groovedRT WING I/B FORE FLAP, CENTER LWR L/E HAS A 1.5 INCH GROOVE WORN INTO SKIN. REMOVED AND REINSTALLED , OPS TEST FLAP IAW A310-200 AMM 27-50-15-4 OPS TEST GOOD. REPAIRED FORE FLAP PER EA 6-5750-89216 AND A310-200 SRM 51-25-00. MAJOR REPAIR IAW FED-EX GMM 6-2SDR ASAA0540278Skin · dentedDENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K)SDR AWXA200500740Skin · delaminatedFOUND DISBOND AREA AT OUTBOARD END OF RT INBOARD AFT FLAP UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DAMAGED AREA ON OUTBOARD END OF RT INBOARD AFT FLAP AND FABRICATED REPAIR DOUBLER AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED FABRICATSDR AWXA200500714Skin · debondedMCN - MAJOR REPAIR - DURING C-13 CHECK FOUND DISBONDED AREA ON UPPER SURFACE OF THE LT INBOARD AFT FLAP 3.0 INCH FROM INBOARD END AT WBL 73 TO WBL 79. MAINTENANCE REMOVED DAMAGED AREA FROM UPPER SURFACE OF THE LT INBOARD AFT FLAP 3.0 INCH FROM INBOARD END AT SDR ASAA0540293Skin · dentedDENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K)SDR ASAA0580300Vane · dentedOKC - FOUND HV-CHECK, RIGHT FLAP VANE DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER. (M)SDR ASAA0580299Vane · gougedOKC - FOUND DURING HV-CHECK, RIGHT FLAP VANE GOUGED. REPAIRED DAMAGED SECTION PER SRM 51-70. (M)SDR P5CA0501361Skin · delaminatedDELAMINATION OF LEADING EDGE OF RT OUTBD FORE FLAP FOUND NOT TO BE WITHIN SRM LIMITS FOR CONTINUED SERVICE. RT OUTBD FORE FLAP REPLACED PER MM 27-51-05.SDR 2006FA0000341Flap · wrong part(ATC0660) DURING ROUTINE MAINTENANCE IT WAS NOTICED THAT THE LT IB AFT FLAP APPEARED TO BE OF THE WRONG TYPE FOR THIS SERIAL OF AIRCRAFT. THE AIRCRAFT IPC WAS CONSULTED AND THIS CONFIRMED THAT TIME 139, AFT FLAP ASSY IS NOT EFFECTIVE FOR THIS AIRCRAFT. A SURSDR AWXA200500761Skin · damagedDURING C-10 CHECK A PYLON STAND HIT RT INBOARD AFT FLAP TRAILING EDGE, DELAMINATING AFT EDGE APPROX 8 INCHES BY 2 INCHES. ALSO, CRACKING LOWER SKIN MEASURING .76 INCHES IN LENGTH EXTENDING FROM AFT EDGE FORWARD LOCATED AT STA 205, BL 21.5L. MAINTENANCE REMOVSDR SWAA051655Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR CA050607008Bracket · cracked(CAN) DO TO A CRACK BEING FOUND ON ONE OF OUR AIRCRAFT, A FLEET CAMPAIGN IS BEING COMPLETED TO INSPECT ALL THE FLAP ACTUATOR ATTACHMENT BRACKETS. DURING THIS SPECIAL INSPECTION, THE LT IB BRACKET WAS FOUND TO HAVE 4 SMALL CRACKS IN THE AREA AROUND THE FWD HOLESDR USAA050718Wedge · crackedCLT - FOUND SKIN CRACKED, RT INBOARD MID FLAP WEDGE. INSTALLED DOUBLR IAW RM 51-70-10. (M)SDR 05FDEA01514Support Bracket · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD CENTER AND AFT BOLT HOLES FOUND CORRODED DURING ACCOMPLISHMENT OF EA 1-5750-83126. REMOVED AND REPAIRED PER FEDEX EA 1-5750-86625.SDR SWAA051634Flap · delaminatedDURING SCHEDULED A2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR C1HA200594002Carriage · vibrationDURING CLIMB-OUT AT APPROX FL 190, VIBRATION FELT THROUGHOUT A/C. VISUAL INSP FOUND LT TE FLAP VIBRATING AS BEFORE (LOG PAGE 3059). VIBRATION PERSISTED FROM 310 KIAS TO 250 KIAS. FUEL DUMPED (APPROX 4000 LBS) AND AIR RETURN TO MMUN. REF LP C03060 ITEM 3. SDR C1HA200594001Roller · out of adjustON CLIMBOUT APPROX 200, CREW BEGAN TO FEEL VIBRATION. ALL ENGINE INDICATIONS NORMAL. BEGAN TROUBLESHOOTING AND UPON VISUAL INSP FOUND LT INBOARD T/E FLAPS FLUTTERING APPROX 4 TO 5 INCHES AT SPEEDS ABOVE APPROX 290 KIAS. DECISION MADE TO AIR RETURN TO MMUN MSDR QXEA200501040Skin · chafedPDX - LEFT WING OUTBOARD FLAP UPPER SURFACE IS CHAFFED AT APPROX YW 271.00 TO YW 265.00, 14" FROM TRAILING EDGE. BLENDED CHAFED AREA IAW DHC-8-400 SRM 57-52-30-320-801 AND REPAIRED IAW HORIZON AIR EA 6-57-437.SDR 05FDEA01498Vane · delaminatedRIGHT HAND WING INBOARD FLAP VANE FOUND DELAMINATED OF ABOUT 57 INCHES LONG BY 28 INCHES WIDE AT LOWER OUTBOARD SURFACE.SDR 05FDEA01479Skin · nickedRIGHT INBOARD FLAP TOP SKIN XIRH 207.30/215.30 RIVETS INSTALLED ON EXISTING NICKS IN SKIN. SKIN TRIMMED REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIG 34 VOL I AND 51-35-01 VOL II. MATERIAL USED AS PER DWG ARC 2369. MAJOR REPAIR AS PER GMM SDR AWXA200500720Skin · debondedDURING C-21 FOUND DISBONDED AREA ON LOWER SURFACE OF RT INBOARD FORE FLAP 11.25 INCHES FROM INBOARD END AND 10 INCHES FROM AFT EDGE. DIMENSIONS OF THE DISBONDED AREA MEASURED 10 BY 8 INCHES MAKING IT OUT OF LIMITS IAW BOEING 737-300 SRM 57-53-021-1 FIG 101. RSDR AWXA200500702Skin · debondedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD FORE FLAP 18 INCHES FROM INBOARD END FROM WBL 206.5 TO WBL 225.2. MAINTENANCE CUT OUT DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD FORE FLAP. FABRICATED REPLACEMENTSDR AWXA200500665Skin · debondedDURING C-21 CHECK, FOUND DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD AFT FLAP, 94 INCHES FROM INBOARD END. MAINTENANCE REMOVED AND CLEANED OUT DAMAGED AREA ON LOWER SURFACE OF LT OUTBOARD AFT FLAP. FABRICATED DOUBLER AND INSTALLED FABRICATED REPAIR PARTS SDR QXEA200501057Skin · chafedRT INBOARD FLAP CHAFED ON INBOARD SIDE TOP SIDE 6 INCHES FROM FUSELAGE. REPAIRED IAW DHC 8 400 SRM 51-14-00 AND HORIZON AIR EA +-57-331.SDR ASAA0540268Skin · delaminatedLT WING OB FORE FLAP DELAMINATED AT IB END. REMOVED DAMAGED AREA OF LT OB FORE FLAP IAW SRM. (K)SDR A6WA200540185Skin · dentedRT IB FLAP LOWER SKIN 4.5 INCH FROM T/E ND 17. INCH FROM IB EDGE. DENT IS 2 INCHES X 2 INCHES X 0.45 INCHES. PERFORMED MAJOR REPAIR BY INSTALLING NON-FLUSH REPAIR IAW SRM. (K)SDR DXTA200500742Guard · looseON TAKEOFF FLAPS (20) WOULD NOT RETRACT TO ZERO. FLAP HANDLE WOULD NOT MOVE FROM DETENT. UPON LANDING AND SHUTDOWN, FLAPS THEN RETRACTED NORMALLY. OPERATED FLAPS NUMEROUS CYCLES AND FOUND NO FAILURE, HOWEVER, FOUND THE FLAP HANDLE SIDE GUARDS LOOSE. REMOVESDR MALA050452Flap Track · wornDURING C1 INSPECTION, FOUND RIGHT FLAP TAB LEADING EDGE WITH WEAR MARKS BEYOND LIMITS UNDER PANEL 641EBSDR 05FDEA01457Skin · nickedLT IB FLAP LOWER SIDE OB SEGMENT XIFH 237.32/266.00 RIVETS INSTALLED ON EXISTING NICKS. LT IB FLAP LOWER SIDE OB SEGMENT XIFH 237.32/266.00 NICKS SKIN. REPAIRED IAW ISRM 57-10-00 FIG 2 VOL I AND SRM 51-35-01 VOL I. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100SDR 05FDEA01441Doubler · misinstalledLT INBOARD FLAP LOWER SIDE INBOARD SEGMENT XIFH 183.30/201.30 RIVETS INSTALLED ON EXISTING SHARP NICKS. LT INBOARD FLAP INBOARD SEGMENT LOWER SIDE DAMAGE AREA FASTENERS. REMOVED AND SKIN TRIMMED. REPAIR SKIN AND 02 EACH SPLICE DOUBLER FABRICATED AND INSTALLSDR VNAA0505009Skin · dentedDURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED A DENT ON THE BOTTOM OF THE LEFT INBOARD FLAP. MAINTENANCE REMOVED & REPLACED THE FLAP IAW CRJ 200 AMM 27-54-01-000-801 AND 27-54-01-400-801. THE SYSTEM WAS RIGGED AND OPERATIONALLY CHECKED GOODSDR A6WA200540181Skin · dentedLT IB FLAP HAS A DENT 22 INCHES FROM IB EDGE AND 14 INCHES FROM THE DENT IS 2 INCH X 2 INCH X 0.55 INCH. LOWER SKIN. PERFORMED A MAJOR REPAIR B4 INSTALLING A 8 INCH X 16 INCH NON-FLUSH REPAIR. (K)SDR SWAA051578Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.SDR CA050526003Bracket · cracked(CAN) DURING A ROUTINE INSPECTION A CRACK WAS NOTICED ON THE LT INBOARD FLAP ACTUATOR ATTACHMENT BRACKET, BRACKET WAS REMOVED AND A TOTAL OF 4 CRACKS WERE FOUND ON THE BRACKET SURROUNDING THE UPPER BOLTHOLE. THE FLAP WAS ALSO CRACKED UNDER THE FORWARD END OF TSDR VNAA0505008Fairing · lightning strikeDURING THE INTERMEDIATE EXTERNAL INSP INBOARD FLAP INBOARD FAIRING AND ON THE LT STABILIZER TIP. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IAW CRJ 700 AMM 05-51-07-220-801-A01. NO OTHER DISCREPANCIES WERE FOUND. THE FLAP FAIRING WAS RSDR USAA050675Skin · gougedCLT - FOUND FLAP SKIN GOUGED 1 INCH BY .5 INCH, TOP SKIN OF RIGHT OUTBOARD FOREFLAP. COMPOSITE REPAIR IAW 737-3 SRM 57-53-02 DETAIL XV, TABLE VI. (M)SDR USAA050674Skin · delaminatedCLT - FOUND FLAP DELAMINATED, .5 INCH BY .5 INCH, LOWER SURFACE OF LT WING INBOARD AFT FLAP. COMPOSITE REPAIR IAW 737 SRM 57-53-02 AND 51-70-10. (M)SDR SWAA051495Skin · delaminatedDURING SCHEDULED RON CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR AWXA200500647Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19, LT INBOARD MID FLAP TRAILING EDGE PANEL 7220 WAS FOUND DELAMINATED AT UPPER AND LOWER SURFACES, APPROX 39 INCHES FROM OUTBOARD EDGE. MAINTENANCE CUT OUT DELAMINATED SKIN AND CORE ON LT INBD MIDFLAP TRL EDGE PANEL UPPER AND LOSDR AWXA200500645Structure · delaminatedDURING C-19 CHECK, THE RT OUTBOARD FLAP INBOARD LOWER CORNER WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGE ON RT OUTBOARD FLAP INBOARD LOWER CORNER, FABRICATED REPAIR CORE AND EXTERNAL DOUBLER, BONDED REPAIR PARTS TO FLAP IAW BOEING SRM 51-70-10 FIG 16.SDR SWAA051469Skin · delaminatedDURING SCHEDULED 5Y CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR QXEA200500992Fitting · wornRT WING TRAILING EDGE OUTBOARD FLAP ROLLER GUIDE FITTING HAS WEAR DAMAGE. REPAIRED IAW CRJ 700 SRM 57-51-02-201-001-A01 AND SRM 51-41-02-001-001-A01.SDR QXEA200500959Flap Track · corrodedPDX - LEFTHAND NR 4 FLAP TRACK FORWARD MOUNT POINT HOLES HAVE SUSPECTED CORROSION. REPAIRED IAW HORIZON AIR EA 6-57-346 AND RD 8/4-57-479.SDR SWAA051449Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR QXEA200500999Vane · chafedRT INBOARD FLAP VANE LEADING EDGE HAS CHAFED MARK. REPAIRED IAW CRJ 700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-00-001-A01.SDR A6WA200540175Skin · dentedRT IB FLAP LOWER SKIN HAS A DENT 2 INCHES X 2.5 INCHES AND .077 INCH DEEP. DENT IS 24 INCHES FROM IB EDGE AND 2 INCHES FROM TRAILING EDGE. REPAIRED RT IB FLAP LOWER SKIN BY INSTALLING FLUSH REPAIR IAW BRAS EO. (K)SDR 05FDEA01360Fairing · crackedLT WING LOWER T/E FLAP TRACK SKATE FAIRING BEHIND MLG STRUT IS CRACKED. REMOVED AND REPLACED SKATE FAIRING IAW SRM 51-30-2.SDR ASAA0580291Skin · gougedOKC - DURING HV CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD LEADING EDGE IS GOUGED. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M)
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