JASC 5753

Service difficulty reports · 31,513

Reports filed under 5753 · Trailing Edge Flaps, newest first.

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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"

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SDR FDEA201205181863Hinge Fitting · corrodedLT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT OTBD MATING SURFACE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1D STEP 1 TO 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.May 18, 2012 · N368FE · Doug MD1010FSDR FDEA201205181849Skin · dentedLT WING OUTER FLAP L/E DENTED APPROX L=12" X W = 4" X D =.46" BETWEEN RIB 17 AND 18 DENT MEASURING L =12" X W = 4" X D =.79" FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00, FIG 101. REPAIRED LT WING OUTER FLAP L/E IAW SRM 57-50-00, FIG 208. OPS CHECKED GOOD IAW May 18, 2012 · N685FE · Airbus A300F4605RSDR FDEA201205181848Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1A STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.May 18, 2012 · N368FE · Doug MD1010FSDR FDEA201205181847Hinge Fitting · corrodedLEFT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT MATING SURFACE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1B, STEP 1 TO 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.May 18, 2012 · N368FE · Doug MD1010FSDR SWAA2012052104195Flap · damagedLEFT WING I/B AFT FLAP DAMAGED. REMOVED AND REPLACED AFT FLAP PER MM.May 17, 2012 · N329SW · Boeing 7373H4SDR DALA1232390121Access Panel · delaminatedRT OTBD TRAILING EDGE FLAP UPPER ACCESS PANEL 666KT DELAMINATED. REPAIRED AS PER SRM 57-53-01, REPAIR 1, FIGURE 201, SHEET 3 AND SRM 51-70-10, REPAIR 4, FIGURE 202, SHEET 3.May 17, 2012 · N121DE · Boeing 767332SDR DALA1232380121Fairing · delaminatedRT WING OTBD TRAILING EDGE FLAP, LEADING EDGE FAIRING DELAMINATED. REPAIRED AS PER SRM 57-53-01, REPAIR 1, TABLE 1 AND SRM 51-70-05 PAR 5A(1), FIGURE 5.May 17, 2012 · N121DE · Boeing 767332SDR DALA1232360121Fairing · delaminatedRT WING OTBD TRAILING EDGE FLAP INBOARD LEADING EDGE FAIRING DELAMINATED. REPAIRED PER SRM 57-53-01, REPAIR 1, TABLE 1 AND SRM 51-70-05 PAR 5A(1), FIGURE 5.May 17, 2012 · N121DE · Boeing 767332SDR DALA1232350121Wedge · delaminatedRT WING OTBD TRAILING EDGE FLAP, LOWER SURFACE WEDGE DELAMINATED. REPAIRED AS PER SRM 57-53-01, REPAIR 1, TABLE II AND SRM 51-70-07, PAR 5A(1), FIGURE 9.May 17, 2012 · N121DE · Boeing 767332SDR SWAA2012052104212Flap · delaminatedLEFT WING O/B FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER AMM.May 16, 2012 · N383SW · Boeing 7373H4SDR QXEA2012051600381Flap Track · wornNR 5 FLAP TRACK WAS WORN AREA IN INBD WEB. REMOVED LOOSE MATERIAL, POLISHED AND BROKE SHARP EDGES IAW RD 8/4-57-1238. REMAINING MATERIAL WITHIN LIMITS IAW RD 8/4-57-1238, COMPLIED WITH STEPS 1-6 OF RD 8/4-57-1238.May 16, 2012 · N424QX · Bombdr DHC8402SDR QXEA2012051600382Flap Track · wornNR 4 LT FLAP TRACK HAS WORN AREA ON INBD WEB. REMOVED LOOSE MATERIAL, POLISHED AND BROKE SHARP EDGES IAW RD 8/4-57-1238. CONFIRMED CRACK FREE AREA REF 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-1238. COMay 16, 2012 · N424QX · Bombdr DHC8402SDR SWAA2012061104816Flap · delaminatedRIGHT WING O/B AFT FLAP DELAMINATED ON INBOARD TRAILING EDGE CORNER. REPAIRED AFT FLAP IAW SRM.May 15, 2012 · N768SW · Boeing 7377H4SDR AALA20120515002Skin · dentedUPPER SKIN DENT 101 INCHES FROM INBOARD END, FIVE INCHES FROM TRAILING EDGE. CUT OUT DAMAGED SKIN, FILLED CORE WITH RESIN AND APPLIED FIBERGLASS WET LAY-UP REPAIR PLIES PER SRM 51-70-17.May 15, 2012 · N694AN · Boeing 757223SDR SWAA2012052104167Skin · delaminatedRIGHT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.May 14, 2012 · N370SW · Boeing 7373H4SDR USAA2012051700009Strut · corroded2S CHECK - CORROSION ON RIGHT WING INTERCONNECTING STRUT ASSEMBLY AT WS 486, RIB 9. REPLACED RIGHT WING INTERCONNECTING STRUT ASSEMBLY AT WS 486, RIB 9 IAW A319 AMM 27-51-44.May 14, 2012 · N733UW · Airbus A319112SDR REXA2012051300658Vane · chafedLT INBD FLAP VANE LEADING EDGE SKIN IS CHAFED AT APPROX WS 56.30. REMOVED AND REPLACED INBOARD FLAP VANE INBOARD LEADING EDGE IAW SRM 51-42-13.May 13, 2012 · N8943A · Cndair CL6002B19SDR SWAA2012051403960Flap · damagedRIGHT WING AFT FLAP INBOARD TRAILING EDGE FLAP DAMAGED. REMOVED AND REPLACED AFT FLAP PER M/M.May 13, 2012 · N902WN · Boeing 7377H4SDR REXA2012051200656Vane · chafedRT WING INBOARD FLAP VANE LEADING IS CHAFED AT APPROX WS 56.30. REMOVED AND REPLACED RT INBOARD FLAP VANE LEADING SKIN IAW SRM 51-42-13.May 12, 2012 · N8943A · Cndair CL6002B19SDR REXA2012051100649Vane · chafedLT INBD FLAP VANE LEADING EDGE CHAFED AT APPROX WS 104. REPAIRED LT INBOARD FLAP VANE LEADING EDGE IAW CRJ 200 SRM 57-52-00.May 11, 2012 · N8943A · Cndair CL6002B19SDR SWAA2012052404306Flap · delaminatedLEFT WING I/B END OF O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.May 11, 2012 · N365SW · Boeing 7373H4SDR FDEA201205111793Bushing · wornLEFT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE ATTACH LOWER BOLT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 0.395" AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72 MAXIMUM ALLOWABLE DIAMETER 0.391". REPAIMay 11, 2012 · N606FE · Doug MD11FSDR FDEA201205111794Bushing · wornWORN BUSHING OF PIVOT HOLE AT RT FORWARD (WING) OTBD FLAP, OTBD HINGE FOR NDT INSPECTION ON PIVOT HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 2.3295" AND MAXIMUM ALLOWABLE DIAMETER 2.3135" FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72May 11, 2012 · N606FE · Doug MD11FSDR SWAA2012051403927Rub Strip · delaminatedLEFT WING REQUIRED EXCESSIVE AILERON TRIM, NOTICED WHEN AUTOPILOT WAS DISCONNECTED AT APPROACH. FOUND RIGHT WING FLAP L/E UPPER RUB STRIP DELAMINATED. REPAIRED FLAP PER MM.May 11, 2012 · N933AT · Boeing 717200SDR FDEA201205111798Skin · gougedGOUGES IN RT OTBD FLAP LOWER SKIN WS 500 CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01, L=1.0" X W=.50" X D=.085". FABRICATED DOUBLER IAW SRM 57-10-00. INSTALLED DOUBLER IAW SRM 51-31-01.May 11, 2012 · N375FE · Doug MD1010FSDR FXGA201205101231Skin · chafedAPPROXIMATELY 8 INCHES OF CHAFING DAMAGE WAS FOUND ON RT FLAP LE. CUT OUT CHAFING DAMAGE. FABRICATE EXTERNAL PATCH FROM 0.020 INCHES 403 STAINLESS WITH ESTABLISHED RIVET PATTERN IAW DC-6A & B OVERHAUL MANUAL FIG 13-47. INSTALL DOUBLER & MS20470AD4 RIVETS WMay 10, 2012 · N351CE · Doug C118ASDR REXA2012051000648Vane · chafedRT WING INBD FLAP VANE LEADING EDGE IS CHAFED AT APPROX WS 104. REPAIRED RT INBOARD FLAP VANE LEADING EDGE IAW CRJ 200 SRM 57-52-00.May 10, 2012 · N8943A · Cndair CL6002B19SDR DALA1230823209Skin · damagedDURING INSPECTION, FOUND LT WING INBD FLAP HAS COMPOSITE DAMAGE ON UPPER SKIN APPROX 5FT FROM INBD END. REPAIRED LT WING INBD FLAP IAW SRM 57-52-00 PARAGRAPH 8F FIG 206.May 10, 2012 · N309US · Airbus A320211SDR SWAA2012051003874Flap · delaminatedAIRCRAFT REQUIRED EXCESSIVE RIGHT WING TRIM ON FINAL TO MAINTAIN DIRECTIONAL CONTROL, TRIM READING 72 PERCENT. FOUND LEFT LEADING EDGE FLAP DELAMINATED. REPAIRED FLAP PER EA.May 10, 2012 · N923AT · Boeing 717200SDR CA120511004Shaft · binding(CAN) AFTER LANDING, FLIGHT CREW SELECTED FLAP 0, FLAPS STARTED TO RETRACT BUT STOPPED AT 12 AND FLAP DRIVE CAUTION LIGHT ILLUMINATED. DURING TROUBLESHOOTING, MAINTENANCE FOUND THE RT WING FLEXIBLE SHAFT ASSY LOCATED BETWEEN THE TORQUE SENSOR AND COUPLING NEAMay 9, 2012 · Dhav DHC8102SDR REXA2012050900646Vane · chafedRT WING INBOARD FLAP VANE LEADING EDGE IS CHAFED AT APPROX WS 139. REMOVED AND REPLACED WITH NEW LEADING EDGE SKIN IAW CRJ 200 SRM 51-42-13.May 9, 2012 · N8943A · Cndair CL6002B19SDR REXA2012050900645Vane · damagedLEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT APPROX WS 139. REMOVED AND REPLACED WITH NEW FLAP VANE LEADING EDGE SKIN IAW SRM 51-42-13.May 9, 2012 · N8943A · Cndair CL6002B19SDR SWIA201230741Vane Cap · chafedRIGHT INBOARD FLAP CENTER LEADING EDGE VANE CAP IS CHAFED. (C-CHECK) REPLACED RIGHT INBOARD FLAP CENTER LEADING EDGE VANE CAP.May 9, 2012 · N629BR · Cndair CL6002B19SDR SWIA201230740Vane Cap · chafedLEFT INBOARD FLAP CENTER LEADING EDGE VANE CAP IS CHAFED. (C-CHECK) REPLACED LEFT INBOARD FLAP CENTER LEADING EDGE VANE CAP.May 9, 2012 · N629BR · Cndair CL6002B19SDR NSVA20120509538Flap · damagedBONDED DUBDLER TO RT UPPER FLAP. REPAIRED IAW TD340-57-11-03 CONTROL=350-62 239-78.May 9, 2012 · N239CJ · Saab 340BSDR AALA20120510014Panel · damagedLEFT AFT INBOARD HAS A HOLE PUNCHED IN FIBER GLASS LEADING EDGE PANEL ON THE UPPER OUTBOARD SIDE. INSTALLED BONDED PERMANENT REPAIR DOUBLERS TO INNER AND OUTER SKIN PER SRM 51-70-04.May 9, 2012 · N613AA · Boeing 757223SDR USAA2012051000002Strut · wornC9 PHASE CHECK - WORN LEFT FLAP INTERCONNECTING STRUT AT WING ZONE 581. REPLACED LEFT FLAP INTERCONNECTING STRUT AT WING ZONE 581 IAW A319 AMM 27-51-44-000-001-A.May 9, 2012 · N754UW · Airbus A319112SDR REXA2012050800644Structure · damagedLEFT INBOARD FLAP TRAILING EDGE DAMAGED. REMOVED DAMAGED AREA AS REQUIRED AND INSTALLED REPAIR IAW SRM 57-52-00.May 8, 2012 · N8943A · Cndair CL6002B19SDR FDEA201205081769Tee Fitting · corrodedRIGHT WING OTBD FLAP VANE TEE FITTING NR 4 FROM INBD FOUND TRACK ATTACH HOLE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02 FIG 201, REV 49. EXISTING SLOT SIZE: 0.885" X 0.613", FINAL SLOT SIZE: 0.978" X 0.743", MAXIMUM ALLOWABLE LIMIT: 0.940"XMay 8, 2012 · N606FE · Doug MD11FSDR USAA2012051400039Strut · corroded2S CHECK - CORROSION ON INNER HOUSING OF INTERCONNECTING STRUT ON LEFT WING AT WS 4862 AT RIB 1 OF THE OUTBOARD FLAP. REPLACED INTERCONNECTING STRUT ON LEFT WING IAW A319 AMM 27-51-44-400-001-A.May 8, 2012 · N733UW · Airbus A319112SDR AALA20120508025Panel · damagedLEFT OUTBOARD MAIN FLAP AFT PANEL HAS HAIL DAMAGE. ACCOMPLISHED BONDED REPAIR PER COMP-57-023331.May 8, 2012 · N653A · Boeing 757223SDR AALA20120508023Panel · damagedRIGHT WING FLAPS AFT PANEL ASSEMBLY HAS HAIL DAMAGE. ACCOMPLISHED BONDED REPAIR PER EA COMP-57-023327.May 8, 2012 · N653A · Boeing 757223SDR AALA20120508026Skin · dentedRIGHT INBOARD FLAP LOWER SURFACE HAS A SMOOTH DENT APPROXIMATELY 6 INCHES BY 9 INCHES BY 0.25 INCH DEEP. SPLICED IN NEW SECTION OF SKIN ON OUTBOARD END OF FLAP WEDGE PER EA MD8057-023631.May 8, 2012 · N9630A · Doug DC983SDR SWAA2012051003886Flap · delaminatedRIGHT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER AMM.May 7, 2012 · N607SW · Boeing 7373H4SDR UALA2012051002691Bushing · damagedRT WING NR 3 FLAP TRACK HAS EXCESSIVE PLAY AT AFT WING ATTACH POINT. REPLACED AFT SPIGOT PIN AND BUSHING PER CMM 57-51-41.May 6, 2012 · N420UA · Airbus A320232SDR UALA2012050802655Structure · damagedLEFT TRAILING EDGE INBOARD FLAP WAS REMOVED FOR ELONGATED HOLE UNDER INBOARD BRACKET ON AFT FAIRING FOR OUTBOARD TRACK. REPAIRED IAW AVO1291.May 6, 2012 · N516UA · Boeing 757222SDR USAA2012051100004Skin · delaminatedC2 CHECK - DELAMINATION ON RIGHT OUTBOARD FOREFLAP LOWER SUREFACE 8 INCHES FROM INBOARD END AT TRAILING EDGE. REPLACED RIGHT OUTBOARD FOREFLAP IAW B737 AMM 27-51-37-401.May 6, 2012 · N530AU · Boeing 7373B7SDR FDEA201205051747Hinge Fitting · corrodedRIGHT WING FLAP SIDE OTBD HINGE, OTBD PIVOT HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA :1.342", FINAL HOLE DIA: 1.354", MAX ALLOWABLE DIA: 1.220" REPAIR ACCOMPLISHED IAW EA 1-5750-160603, PART 1. REPAIR May 5, 2012 · N607FE · Doug MD11FSDR FDEA201205051746Hinge Fitting · corrodedRIGHT WING FLAP SIDE OTBD HINGE, INBD PIVOT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA :1.378" , FINAL HOLE DIA: 1.388" MAX.ALLOWABLE DIA.: 1.220" REPAIR ACCOMPLISHED EA 1-5750-160603, PART 1. REPAIR CLASMay 5, 2012 · N607FE · Doug MD11FSDR FDEA201205051745Hinge Fitting · corrodedLEFT WING FLAP SIDE HINGE FITTING, OTBD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03, REV 72, EXISTING HOLE DIA: 1.2575", FINAL HOLE DIA: 1.288" , MAX ALLOWABLE DIA: 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-160604May 5, 2012 · N607FE · Doug MD11F
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