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"

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SDR 08FDEA03271Rub Strip · wornRIGHT INBD FLAP L/E NOSE SKIN STRAPS HAVE ELONGATED HOLES, (2 STRAPS) MATERIAL ID IAW A300-600 SRM 51-31-00. FABRICATED, LOCATED AND DRILLED IAW A300-600 SRM 51-40-44. ALODINED AND PRIMED IAW A300-600 SRM 51-21-10.Aug 5, 2008 · N728FD · Airbus A300B4622RSDR SWAA084367Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT UPPER AND LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM.Aug 5, 2008 · N650SW · Boeing 7373H4SDR 08FDEA03239Skin · dentedRIGHT WING INBD FLAP UPPER SKIN IS DENTED 5' FROM THE INBD END. SMOOTHED AREA AROUND THE DENT IAW A300-600 SRM 51-73-10. ORIGINAL MATERIAL 0.031 IAW SRM 57-52-12; ITEM 45. MATERIAL REMOVED 0.002. MATERIAL REMAINING 0.029, FOUND TO BE OUT OF LIMITS IAW AAug 4, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03238Skin · gougedRIGHT WING INBD FLAP UPPER SKIN 1 INCH FROM THE INBD END IS GOUGED. BLENDED GOUGE IAW A300-600 SRM 51-73-10. ORIGINAL MATERIAL THICKNESS 0.031 IAW A300-600 SRM 57-52-12; ITEM 45. REMOVED 0.004. REMAINING MATERIAL 0.027 AND FOUND TO BE OUT OF LIMITS IAW AAug 4, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03235Skin · dentedLEFT WING INBD FLAP LOWER SURFACE IS DENTED INBD OF THE FLAP TRACK. UPON FURTHER INVESTIGATION THE DENT WAS FOUND TO BE GOUGED. BLENDED GOUGE SMOOTH IAW SRM 51-73-10. FLAP SKIN WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00; PG 108. REPAIRED LOWER SKIN IAug 4, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03244Skin · gougedRIGHT WING INBD FLAP LOWER T/E SKIN IS GOUGED 7' FROM THE INBD END. REMOVED GOUGE IAW SRM 51-73-10. ORIGINAL MATERIAL 0.028 IAW SRM 57-50-00. MATERIAL REMOVED 0.015. MATERIAL REMAINING 0.013. FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. REPAIRED AREA IAAug 4, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03242Skin · dentedRIGHT WING INBD FLAP LOWER SKIN HAS SEVERAL DENTS. SMOOTHED DENTS IAW SRM 51-73-10. ALL DENTS EXCEPT RIB 7. ORIGINAL MATERIAL IS 0.028. MATERIAL REMOVED 0.015. MATERIAL REMAINING 0.013; FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. RIB 7 DENT 0.049 DEPTH.Aug 4, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03241Skin · dentedRIGHT WING INBD FLAP UPPER SKIN IS CREASED 3' FROM THE OUTBD END. SMOOTHED DENT IAW SRM 51-73-10. DENT DEPTH 0.049. ORIGINAL MATERIAL THICKNESS IS 0.031. NO MATERIAL LOSS NOTED, FOUND TO BE WITHIN LIMITS IAW SRM 57-50-00, FIG 101. DENT DIAMETER 1.25 INCH, Aug 4, 2008 · N664FE · Airbus A300F4605RSDR 08FDEA03234Skin · dentedLEFT WING INBD FLAP LOWER SURFACE IS DENTED INBD OF THE FLAP TRACK. DENT WAS FOUND TO BE GOUGED. BLENDED GOUGE SMOOTH IAW A300-600 SRM 51-73-10. FLAP SKIN FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00, PG 108. CUT OUT THE DAMAGED AREA IAW A300-600 SRAug 4, 2008 · N664FE · Airbus A300F4605RSDR ASAA0843340Skin · dentedLT OUTBOARD T/E AFT FLAP HAS NUMEROUS DENTS ON THE LOWER SURFACE. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER & BONDED THE REPAIR PARTS IAW B737 400 SRM 51 70 10 REPAIR 4.Aug 3, 2008 · N706AS · Boeing 737490SDR ASAA0843335Skin · chafedRT INBOARD AFT FLAP UPPER SURFACE IS CHAFED AT WBL 82. PREPPED DAMAGED AREA, FABBED DOUBLER & BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2.Aug 3, 2008 · N706AS · Boeing 737490SDR SWAA084312Flap · delaminatedDURING SCHEDULED 8Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.Aug 3, 2008 · N776WN · Boeing 7377H4SDR FDEA200808013208Skin · crackedLT WING OTBD FLAP FOUND CRACKS ON LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 65 VOL I.Aug 1, 2008 · N318FE · Doug DC1030FSDR 2008FA0000558Fitting · corrodedTHE PART WAS BEGINNING TO RUST THROUGH IN LOCATION RESPONSIBLE FOR ATTACHING THE LT FLAP TO THE FLAP CONTROL. THE DEFECT WAS FOUND DURING AN ANNUAL INSPECTION. PROBABLE CAUSE WAS RUSTING DUE TO AGE. A MORE THOROUGH INSPECTION OF THE AREA DURING PREFLIGHT SHOULAug 1, 2008 · N76671 · Cessna 140SDR UIEA2008002272Skin · chafedLEFT WING INBOARD FLAP, AFT FLAP S/N 000204 UPPER SKIN HAS 4 EACH AREAS OF CHAFING CAUSED BY LONG BOLTS ON MID-FLAP. AREAS ARE WBL 248.0, 297.0, 339.0 AND 425.0. CHAFE IS .500 INCH IN DIAMETER. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG Aug 1, 2008 · N506MC · Boeing 7472D3BSDR SWAA084299Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.Aug 1, 2008 · N621SW · Boeing 7373H4SDR 08FDEA03199Skin · dentedRIGHT WING INBD FLAP LOWER SKIN SURFACE HAS AREAS OF DENTS. FABRICATED A NEW SKIN PANEL ASSEMBLY IAW EA NR 8-5750-118534.Jul 31, 2008 · N372FE · Doug MD1010FSDR UPS08853081Doubler · gougedINSPECTION TYPE:C1 RT WING O/B FLAP STA XF 228 HAS A ROUND DOUBLER GOUGED AT UPPER SKIN, NEXT TO L/E AREA. REMOVED EXISTING DOUBLER IAW SRM 51-1-21A. FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW SRM 57-07-01 FIG 004, 57-02-0 FIG 002A, AND SRM 51-1Jul 30, 2008 · N715UP · Doug DC871FSDR MAL2008F00027Rib · crackedRT FLAP, AFT COVE RIB CRACKED. INSTALLED NEW RT FLAP AFT COVE RIB IAW SRM 51-20-00 AND 51-40-00 AND EOS57051. REPLACED FASTENERS IN RT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR - ALJul 30, 2008 · N448XJ · Saab 340BSDR MAL2008F00025Rib · crackedLT FLAP, AFT COVE RIB CRACKED AND MISSING RIVET. INSTALLED NEW AFT COVE RIB P/N 7257840081. IAW SAAB340 SRM 51-40-22 AND EOS57051. REPLACED FASTENERS IN LT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING AFT BULKHEAD UPPER FLJul 30, 2008 · N448XJ · Saab 340BSDR UPS08852993Skin · gougedINSPECTION TYPE:C1, RT WING OB FLAP STA XF 228 HAS EXISTING REPAIR DOUBLER GOUGED AT UPPER FLAP SKIN, NEXT TO AFT FIXED PANEL OF FLAP HINGE COVER REMOVED EXISTING DOUBLER FABRICATED AND REPLACED REPAIR DOUBLER IAW SR M 51-1-21A, 57-2-8 FIG 2A,57-7-01 FIG 4Jul 30, 2008 · N715UP · Doug DC871FSDR MAL2008F00021Fastener · unknownREPLACED FASTENERS IN LT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR - ALTERNATIVE FASTENER REPLACEMENT AUTHORIZATION. STANDARD SRM REPAIR PROCEDURES. NO INFORMATION ON THE PART CONDIJul 30, 2008 · N448XJ · Saab 340BSDR MAL2008F00020Flap · dentedRT FLAP HAS A DENT AT WS 42.4, TOP INBOARD EDGE. REPAIRED IAW EOS51031. THIS EO PROVIDES A GENERIC COLD BOLD (WET LAYUP) REPAIR IAW SAAB SRM 51-70-50. (S)Jul 30, 2008 · N448XJ · Saab 340BSDR MAL2008F00019Fastener · unknownREPLACED FASTENERS IN RT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR - ALTERNATIVE FASTENER REPLACEMENT AUTHORIZATION. STANDARD SRM REPAIR PROCEDURES. NO INFORMATION ON THE PART CONDIJul 30, 2008 · N448XJ · Saab 340BSDR 2008FA0000538Spar · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)Jul 30, 2008 · N742VA · Boeing 737448SDR 2008FA0000514Spar · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)Jul 30, 2008 · N742VA · Boeing 737448SDR 2008FA0000513Spar · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)Jul 30, 2008 · N742VA · Boeing 737448SDR 08FDEA03172Skin · chafedRT WING CENTER FLAP UPPER SURFACE APPROX RIB 16, 7 EA WEAR MARKS FROM BUTTON HEAD RIVETS CHAFING REMOVED DAMAGED SECTION AND INSTALLED FLAP SKIN PATCH REPAIR IAW SRM 57-50-00, FIG 205, PG 219.Jul 30, 2008 · N686FE · Airbus A300F4605RSDR 08FDEA03161Skin · gougedT/E OF LT OB FOREFLAP HAS (2) EA DEEP GOUGES ON UPPER SURFACE. REMOVED DAMAGED AREA IAW SRM 51-40-20 PAGE 12. FABRICATED FILLER AND DOUBLER IAW SRM 51-40-20 PAGE 59. HOT BONDED FILLER AND DOUBLER ON SEALED EDGES AND PRIMED AREA IAW SRM 51-40-20 PARAGRAPH 7-Jul 30, 2008 · N275FE · Boeing 727233SDR UPS08853157Skin · wornINSPECTION TYPE:C1 2 WORN AREAS EITHER SIDE OF O/B FLAP STA 340 LT FLAP. FABRICATED AND INSTALLED REPAIR DOUBLER ON O/B SIDE OF STA 340 IAW SRM 57-07-01 AND 51,1-21A.Jul 29, 2008 · N715UP · Doug DC871FSDR UPS08852994Structure · damagedINSPECTION TYPE:C1, TWO HOLES IN LT FLAP EITHER SIDE OF FLAP STATION 219 BACKSIDE OF FLAP. CUT OUT DAMAGE, FABRICATED AND INSTALLED 2EA REPAIR DOUBLERS IAW SRM 5 7-02-01 FIG 2Q,51-01-09, AND 51-01-21AJul 29, 2008 · N715UP · Doug DC871FSDR 08FDEA03136Skin · gougedTHE LEFT WING CENTER FLAP UPPER SKIN IS GOUGED. AREA IS OUT OF LIMITS IAW SRM 57-50-00; FIG 102; SHEET 5. FABRICATED IAW SRM 57-50-00; PG 219. ALODINED AND PRIMED IAW AMM 51-22-00-0, PG 1. INSTALLED IAW SRM 57-50-00, PG 219.Jul 29, 2008 · N728FD · Airbus A300B4622RSDR CALA0800752Torque Tube · corrodedLEFT INBOARD MIDFLAP PART NUMBER 65C26310-25, S/N BN1835 BOTH INBOARD AND OUTBOARD CARRIAGES AND TORQUE TUBES CORRODED BEYOND LIMITS. PARTS REPLACED: CARRIAGE HALFS 65-52246-15 /-17, CARRIAGE ASSY 65-47856-13 /-14, TORQUE TUBES 65-52211-1 /-2, 69-37206-14.Jul 29, 2008 · N32626 · Boeing 737524SDR CALA0800751Gimbal Joint · corrodedRIGHT INBOARD MIDFLAP PART NUMBER 65C26310-26, S/N BN1829 BOTH INBOARD AND OUTBOARD CARRIAGES, TORQUE TUBES AND ONE GIMBAL CORRODED BEYOND LIMITS. PARTS REPLACED: CARRIAGE HALF'S 65-52246-16, S/N 12142, 65-52246-18, S/N 11485, 65C26343-3, S/N 12635, GIMBAL (Jul 29, 2008 · N32626 · Boeing 737524SDR SWAA084211Flap Track · corrodedDURING SCHEDULED BRDG CHECK, FOUND RT WING NR 2 T/E AFT FLAP AFT ATTACH POINT CORRODED. REMOVED AND REPLACED FLAP TRACK PER SWA EA.Jul 28, 2008 · N336SW · Boeing 7373H4SDR USAA920081453Flap · delaminatedCLT-C2-MAJOR REPAIR - 11 INCH SPLIT AT INBOARD TRAILING EDGE AND 2 AREAS OF DELAMINATION ON LT OUTBOARD FOREFLAP. REPLACED LT OUTBOARD FOREFLAP IAW B737 AMM 27-51-37. (S)Jul 27, 2008 · N432US · Boeing 7374B7SDR SWAA084141Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RIGHT WING INBOARD FORE FLAP OUTBOARD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Jul 27, 2008 · N328SW · Boeing 7373H4SDR 08FDEA03079Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE SKIN HAS MULTIPLE DENTS INBD OF THE SPRING CARTRIDGE. CHECKED DENTS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00; VOL I; FIG 48 AT STA XIFH 250 AT 254. REMOVED THE LOWER SKIN WEDGE SKIN IAW SRM 51-35-02; VOL II. RECEIVEDJul 25, 2008 · N372FE · Doug MD1010FSDR CALA0800744Skin · delaminatedLEFT OUTBOARD AFT FLAP HAS A DELAMINATED AREA ON LOWER INBOARD SURFACE. REMOVED LEFT OUTBOARD AFT FLAP PER MM 27-51-39, REPAIRED PER SRM 51-70-10, REINSTALLED LEFT OUTBOARD AFT FLAP PER MM 27-51-39.Jul 25, 2008 · N16647 · Boeing 737524SDR SWAA084120Skin · debondedDURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DSBONDED AT OUTBOARD END. R&R FLAP PER MM.Jul 24, 2008 · N648SW · Boeing 7373H4SDR 2008FA0000630Hinge Bracket · corrodedLT FLAP OB HINGE BRACKET, SEVERE CORROSION AT IB AND OB SUPPORTING RIBS WHERE HINGE BRACKET JOINS FLAP. UNABLE TO PERFORM VISUAL INSPECTION OF AREA AS DAMAGE IS CONCEALED BY SKIN. (K)Jul 23, 2008 · N278D · Beech 76SDR 2008FA0000627Hinge Bracket · corrodedLT FLAP OB HINGE BRACKET, SEVERE CORROSION AT IB AND OB SUPPORTING RIBS WHERE HINGE BRACKET JOINS FLAP. UNABLE TO PERFORM VISUAL INSPECTION OF AREA AS DAMAGE IS CONCEALED BY SKIN. (K)Jul 23, 2008 · N6708A · Beech 76SDR 2008UALA03921Skin · damagedRT WING O/B FLAP HAS A REPAIR OF 8 INCHES BY 15 INCHES ON LOWER TRAILING EDGE. THE TRAILING EDGE OF REPAIR IS SEPARATING FROM FLAP. *S/D* REPAIRED FLAP.Jul 23, 2008 · N433UA · Airbus A320232SDR MAL2008F00017Skin Panel · dentedTHREE DENTS WERE FOUND ON RT FLAP UPPER SKIN PANEL 641AT FROM WS 94.5 TO WS 99. DENTS WERE REPAIRED IAW EOS57201. (S)Jul 23, 2008 · N403XJ · Saab 340BSDR MAL2008F00016Skin · damagedDURING INSTALLATION OF RT FLAP DAMAGE OCCURRED TO THE LEADING EDGE AT WS 174.3. DAMAGE WAS REPAIRED IAW EO57204 AND EO57060. (S)Jul 23, 2008 · N403XJ · Saab 340BSDR MAL2008F00014Structure · damagedFLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR FASTENERS. REPLACED IAW EOS57051. (S)Jul 23, 2008 · N403XJ · Saab 340BSDR 08FDEA03025Fitting · crackedRT WING OUTBD FLAP CRACK ON FITTING. REPAIRED AREA IAW EA 8-5750-120139.Jul 23, 2008 · N40061 · Doug DC1010SDR 2008FA0000629Hinge Bracket · corrodedLT FLAP OB HINGE BRACKET, SEVERE CORROSION AT IB AND OB SUPPORTING RIBS WHERE HINGE BRACKET JOINS FLAP. UNABLE TO PERFORM VISUAL INSPECTION OF AREA AS DAMAGE IS CONCEALED BY SKIN. (K)Jul 22, 2008 · N110SU · Beech 76SDR 2008FA0000628Hinge Bracket · corrodedLT FLAP OB HINGE BRACKET, SEVERE CORROSION AT IB AND OB SUPPORT RIBS, WHERE HINGE BRACKET PIN FLAP. UNABLE TO PERFORM VISUAL INSPECTION OF AREA AS DAMAGE IS CONCEALED INSIDE OF SKIN. (K)Jul 22, 2008 · N6638D · Beech 76SDR UPS08152975Skin · chafedINSPECTION TYPE:5 YR, RT WING OB FLAP L/E IB CHAFED. REPAIRED RT WING OB FLAP L/E IB SIDE REF A-300-600 SRM 57-50-0 0 FIG 208.Jul 22, 2008 · N153UP · Airbus A300F4622R
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