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.

SDR IPXA2020072768243Hinge · corrodedINSPECTION TYPE:S/V, RT OTBD FLAP OTBD FWD HINGE O/B LWR STUD MOUNT HOLE HAD CORROSION. REPAIRED THE FLAP O/B HINGE IAW EA 011-5740-01-A8439, REV I/R, AND EO MD11-5740-77319-A. MINORJul 26, 2020 · N273UP · Doug MD11FSDR IPXA2020072768242Hinge · corrodedINSPECTION TYPE:S/V, RT OTBD FLAP FWD HINGE INBD LWR STUD MOUNT HOLE HAD SURFACE CORROSION. REPAIRED THE FLAP HINGE STUD MOUNT IAW CMM 57-44-09 REPAIR 1-1.Jul 26, 2020 · N273UP · Doug MD11FSDR FDEA2020072761660Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11FSDR FDEA2020072761659Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11FSDR FDEA2020072761658Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11FSDR FDEA2020072761657Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11FSDR FDEA2020072761656Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11FSDR FDEA2020072761655Hinge Fitting · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11FSDR SWIA2020090452214Skin · dentedRT INBOARD FLAP UPPER SKIN HAS DENTS AT WS 73 10" FROM TRAILING EDGE AND WS 76 14" FROM TRAILING EDGE. EVALUATE AND REMOVE DAMAGE, OR FILL AND PAINT. C-CHECK RO 9/1/2020. REPAIRED RT INBOARD FLAP UPPER SKIN, REF CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAJul 24, 2020 · N445SW · Cndair CL6002B19SDR FDEA202007241641Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-Jul 24, 2020 · N585FE · Doug MD11FSDR FDEA202007241640Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09Jul 24, 2020 · N585FE · Doug MD11FSDR SWIA2020090452278Angle · bentLT INBOARD FLAP FWD RIB, BOTTOM RIB ANGLE BENT UP AND NOT SECURED. RIB IS ON THE INBOARD SIDE OF THE OUTER HINGE ARM. REMOVED AND INSTALLED SERVICEABLE LT INBOARD FLAP, REF CRJ 200 AMM. PERFORMED OPERATIONAL TEST OF THE FLAPS IAW CRJ 200 AMM, TEST GOOD.Jul 23, 2020 · N445SW · Cndair CL6002B19SDR FDEA202007231630Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SJul 23, 2020 · N585FE · Doug MD11FSDR FDEA202007231631Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- Jul 23, 2020 · N585FE · Doug MD11FSDR FDEA202007231625Skin · gougedLEFT WING INBD FLAP UPPER SURFACE, OTBD SIDE HAD A DEEP GOUGE. COMPLIED WITH EA:6-5752-123008 B P3. MAJOR REPAIR IAW GMM 6-2-100.Jul 23, 2020 · N742FD · Airbus A300B4622RSDR SWIA2020090152094Vane · chafed* R/H INBD FLAP VANE - FLAP VANE CHAFFED AT OUTERMOST WEAR PAD LOCATION (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED R/H INBD FLAP VANE REF. CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.Jul 22, 2020 · N463SW · Cndair CL6002B19SDR IPXA2020072258090Angle · crackedINSPECTION TYPE:4C, LT OTBD FLAP, INBD HINGE FAIRING TEE ANGLE CRACKED AT THE INBD SIDE. REMOVED AND REPLACED THE TEE ANGLE IAW SRM 51-35-01, AND 51-33-01. MINOR.Jul 22, 2020 · N292UP · Doug MD11FSDR IPXA2020072258089Support Angle · crackedINSPECTION TYPE: 4C, LEFT OTBD FLAP INBD HINGE AFT FAIRING SUPPORT ANGLE WAS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-31-01. MINORJul 22, 2020 · N292UP · Doug MD11FSDR SWIA2020090452204Vane · chafedRT INBOARD FLAP VANE SKIN CHAFED AT THE CENTER OF THE LEADING EDGE. C-CHECK RO 9/1/2020. REMOVED AND REPLACED WITH NEW RT INBOARD FLAP CENTER VANE SKIN, REF CRJ 200 SRM AND BOMBARIDER DWG. COMPLIED WITH SKYWEST TASK CARD.Jul 21, 2020 · N445SW · Cndair CL6002B19SDR SWIA2020090152126Cleat · cracked* THE LH INBD FLAP VANE FRONT SPAR OUTBD SIDE CLEAT IS CRACKED. (MARKED) (C-CHECK) RO 8/28/2020 REMOVED LH INBD FLAP AND INSTALLED NEW SERVICEABLE FLAP. REF CRJ 200 AMM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.Jul 21, 2020 · N463SW · Cndair CL6002B19SDR SWIA2020090152093Hinge · gouged* L/H OBD FLAP INB HINGE BOX AFT ATTACHMENT FITTING ON WING HAS INB LUGS GOUGED AT INB CORNERS. (C-CHECK) RO 8/28/2020 BLENDED OUT GOUGES ON LH OB FLAP IB HINGE BOX IB LUGS REF MHIRJ REO, ALL STEPS COMPLIED WITH AND RESTORED THE FINISH. NO WEIGHT STATEMENJul 21, 2020 · N463SW · Cndair CL6002B19SDR SWIA2020090152092Vane · chafed* THE LH INBD FLAP VANE LEADING EDGE IS CHAFFED JUST OUTBD OF THE #3 FLAP VANE ACTUATOR. (MARKED) (C-CHECK) RO 8/28/2020 BLENDED OUT CHAFE DAMAGE ON THE LH INBD FLAP VANE LEADING EDGE, JUST OUTBD OF THE #3 FLAP VANE ACTUATOR REF CRJ-200 SRM. ORIGINAL THJul 21, 2020 · N463SW · Cndair CL6002B19SDR SWIA2020090152091Vane · chafed* THE LH INBD FLAP VANE LEADING EDGE IS CHAFFED JUST INBD OF THE #1 FLAP VANE ACTUATOR. (MARKED) (C-CHECK) RO 8/28/2020 BLENDED OUT CHAFE DAMAGE ON LH INBD FLAP VANE JUST INBD OF #1 FLAP VANE ACTUATOR IAW CRJ200 SRM. ORIGINAL THICKNESS OF LH IB FLAP VANEJul 21, 2020 · N463SW · Cndair CL6002B19SDR FDEA202007211609Skin · crackedFOUND RH CENTER FLAP CRACKED AT RIB 17 APPROX 5" AFT OF FRONT SPAR LOWER SKIN. AFTER FURTHER INVESTIGATIONI OF X-RAY FILM AND BORESCOPE OF THE SUSPECTED AREA AREA, NO CRACK WAS NOTED ON RIB 17 OF THE RH FLAP. CUT LOWER SKIN 6" X 3" FOR ACCESS IAW SRM 57-5Jul 21, 2020 · N676FE · Airbus A300F4605RSDR FDEA2020072311601Skin · dentedLEFT WING INBOARD FLAP DENTED OUTBOARD END. REPAIRED THE LT WING INBD FLAP IAW EA H-5750-T0355223-P1.Jul 21, 2020 · N126FE · Boeing 7673S2FSDR AALA2020072319013Flap · crackedAIRCRAFT IN BASE MAINTENANCE, RIGHT WING OUTBOARD FLAP FOUND CRACKED. REMOVED AND REPLACED RIGHT WING OUTBOARD FLAP IAW AMM 27-54-62. ADJUSTED FORWARD ECCENTRIC BEARING, OKAY. CHECKED SPOILER DIMENSION IAW AMM 27-64-00-820-001-C, WITHIN LIMITS. PERFORMED Jul 20, 2020 · N668AW · Airbus A320232SDR AALA2020072219012Bolt · seizedAIRCRAFT IN BASE MAINTENANCE: THE RIGHT WING TRAILING EDGE OUT BOARD FLAP HAS A SIEZED BOLT IN THE ATTACMENT FITTING THAT CONNECTS THE OUTBOARD FLAP TO THE OUTBOARD FLAP TRACK CARRIAGE ASSEMBLY. REMOVED AND REPLACED BOLT PER AMM 27-54-62-000-001-A STEP 4.C (6Jul 20, 2020 · N833AW · Airbus A319132SDR AALA2020072219011Bolt · seizedAIRCRAFT IN BASE MAINTENANCE, THE RIGHT WING TRAILING EDGE OUT BOARD FLAP HAS A SEIZED BOLT IN THE ATTACMENT FITTING THAT CONNECTS THE OUTBOARD FLAP TO THE INBOARD FLAP TRACK CARRIAGE ASSEMBLY. REMOVED AND REPLACED BOLT PER AMM 27-54-62-000-001-A STEP 4.C (Jul 20, 2020 · N833AW · Airbus A319132SDR SWIA2020090952414Spring · corrodedRT OB FLAP HINGE BOXES SPRINGS AT WS 178.00, WS 220.00, AND WS 264.00 ARE CORRODED. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE HARDWARE ON HINGE BOX SPRINGS AT WS 178.00, 220.00, AND 264.00, IAW CRJ 200 AMM. PERFOMRED OPS TEST, OPSJul 18, 2020 · N910SW · Cndair CL6002B19SDR SWIA2020090952413Spring · corrodedLT OB FLAP HINGE BOXES SPRINGS AT WS 178.00, WS 220.00 AND 264.00 ARE CORRODED. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE HINGE BOX HARDWARE AT WS 178.00 AND 264.00, IAW CRJ 200 AMM. PERFORMED OPS TEST, OPS TEST GOOD. SEE ATTACHEJul 18, 2020 · N910SW · Cndair CL6002B19SDR SWIA2020090452268Vane · crackedCRACK ON OUTBOARD MOVEABLE FLAP VANE AT APPROXIMATELY WS 226.51 TRAILING EGDE. REMOVED AND REPLACED RT OUTBOARD FLAP, REF CRJ200 AMM. ALL ASSOCIATED OPERATIONS CHECKS GOOD.Jul 18, 2020 · N445SW · Cndair CL6002B19SDR SWIA202090252194Bracket · chafedRT WING INBOARD TRAILING EDGE, I/B FLAP STUB FAIRING MOUNTING BRACKET CHAFED APPOX. 0.025 DEEP. C-CHECK RO 8/29/2020. REMOVED DAMAGED RT WING I/B TRAILING EDGE FLAP STUB FAIRING MOUNTING BRACKET AND INSTALLED NEW SERVICEABLE MOUNT BRACKET IAW CRJ 200 SRM.Jul 18, 2020 · N917EV · Cndair CL6002B19SDR IPXA2020080558660Panel · dentedINSPECTION TYPE:C2, DENT WAS FOUND ON THE LOWER PANEL ASSY OF R/H INBD T.E AFT FLAP NEAR WBL 182.REPAIR I.A.W. SRID: 4-4824467363 AND EO B747-5750-77402-A.Jul 18, 2020 · N572UP · Boeing 74744AFSDR IPXA2020072438143Angle · crackedINSPECTION TYPE:2CLT WING I/B FLAP I/B FWD HINGE FAIRING O/B "T" ANGLE IS CRACKED.REMOVED AND REPLACED CRACKED LT WING I/B FLAP I/B FWD HINGE FAIRING O/B "T" ANGLE IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)Jul 18, 2020 · N292UP · Doug MD11FSDR FDEA2020071761552Skin · crackedFOUND A CRACK ON THE RT CENTER FLAP AT RIB 18, APPROX 5 INCHES FWD OF REAR SPAR ON UPPER SKIN. CUT THE SKIN ON LOWER SURFACE FOR ACCESS AND REPAIRED THE CRACK IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER IAW SRM 57-50-00, FIG 205. CATAGORY A MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605RSDR FDEA2020071761551Skin · crackedFOUND A CRACK ON THE RT CENTER FLAP, AT RIB 16 APPROX 4.8 INCHES FWD OF REAR SPAR UPPER SKIN. CUT THE SKIN ON LOWER SURFACE FOR ACCESS AND REPAIRED THE CRACK IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER IAW SRM 57-50-00, FIG 205. CATAGORY -A- MAJOR REPAIRJul 16, 2020 · N676FE · Airbus A300F4605RSDR FDEA2020071761550Skin · crackedFOUND A CRACK ON THE RT CENTER FLAP AT RIB 12, APPROX 5.1 INCHES FWD OF REAR SPAR, ON UPPER SKIN. ACCESSED AND REPAIRED THE DAMAGE IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER ON THE LOWER SKIN IAW SRM 57-50-00, FIG 205, AND SRM 51-40-21. CATAGORY -A- MAJul 16, 2020 · N676FE · Airbus A300F4605RSDR FDEA2020071761549Skin · crackedFOUND A CRACK ON THE RT CENTER FLAP AT RIB 11, LOCATED APPROX 5 INCHES FWD OF REAR SPAR IN THE UPPER SKIN. ACCESSED AND REPAIRED THE DAMAGE IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER ON LOWER THE SKIN IAW SRM 57-50-00, FIG 205, AND SRM 51-40-21. CATAGOJul 16, 2020 · N676FE · Airbus A300F4605RSDR IPXA2020081459052Skin · delaminatedINSPECTION TYPE:3CL/H WING O/B FLAP I/B T/E IS DELAMINATED BETWEEN STA. XOF= 574 TO 495.REPAIRED DELAMINATED L/H WING O/B FLAP IAW VT-SAA EA 011-5753-01-A8455 REV. I/R AND UPS EO MD11-5750-77481-A. (MINOR)Jul 15, 2020 · N279UP · Doug MD11FSDR IPXA2020081098813Angle · crackedINSPECTION TYPE:C3, LT WING O/B FLAP I/B AFT HINGE FAIRING I/B LOWER T ANGLE IS CRACKED,REPLACED CRACKED T ANGLE AT LT WING O/B FLAP I/B AFT HIMGE IAW SRM 51-31-01. (MINOR)Jul 15, 2020 · N279UP · Doug MD11FSDR IPXA2020081078772Vane · delaminatedINSPECTION TYPE:C3, RT INBD FLAP VANE HAD FOUR AREAS OF DELAMINATION AT LOWER SURFACE. REPLACED DELAMINATED FLAP VANE IAW AMM 27-50-22.Jul 15, 2020 · N279UP · Doug MD11FSDR IPXA2020080318510Wedge · delaminatedINSPECTION TYPE:C3, LEFT WING OTBD FLAP T/E WEDGE INBD SECTION HAD A LARGE AREA OF DELAMINATION. REPAIRED THE FLAP T/E WEDGE IAW 57-50-80, REPAIR 1, 6" X 5.75" PERMANENT REPAIR. (MINOR)Jul 15, 2020 · N279UP · Doug MD11FSDR 120B2020071500098Skin · delaminatedLH INBD UPPER FLAP, INTERNAL SKIN HAS COMPOSITE DELAMINATION (REPAIRED).Jul 15, 2020 · N36NE · Boeing 767323SDR 120B2020071500097Seal · wornFLAP FAIRING PANEL 61AB HAS A WORN SEAL.Jul 15, 2020 · N36NE · Boeing 767323SDR 120B2020071500096Bushing · missingFLAP FAIRING PANEL 671AB HAS A BUSHING MISSING FROM THE MOUNTING BRACKET.Jul 15, 2020 · N36NE · Boeing 767323SDR FDEA2020073041510Rib · crackedFOUND CRACK ON RT CTR FLAP AT RIB 27 APPROX. 4.8" FWD OF REAR SPAR UPPER SKIN. REPAIRED RIB FLANGE IAW SRM 57-50-00, FIG. 205, CAT A MAJOR REPAIR.Jul 14, 2020 · N676FE · Airbus A300F4605RSDR 120B2020071400076Seal · tornINBD FLAP FAIRING PANEL 671DB HAS A TORN SEAL.Jul 14, 2020 · N36NE · Boeing 767323SDR 120B2020071300070Housing · wornFLAP TORQUE TUBE CARRIER BEARING HAS UP & DOWN PLAY IN THE HOUSING (LH SIDE).Jul 13, 2020 · N36NE · Boeing 767323SDR AALA2020081109028Skin · delaminatedAIRCRAFT WAS GROUNDED: LEFT WING TRAILING EDGE OUTBOARD FLAP TRAILING EDGE WEDGE DELAMINATED. REPAIRED FLAP PER EA 307258A.Jul 11, 2020 · N809AW · Airbus A319132SDR AALA2020071329006Skin · delaminatedAIRCRAFT WAS GROUNDED: LEFT WING TRAILING EDGE OUTBD FLAP TRAILING EDGE WEDGE DELAMINATED. REPAIRED THE FLAP PER EA 307258A.Jul 11, 2020 · N809AW · Airbus A319132
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