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 08FDEA03001Panel · wornRIGHT WING OUTBOARD FLAP PANEL 636 AR HAS SEVERAL DENTS. REMOVED THE SKIN AND CORE IN THE DAMAGED AREA. MATERIAL ID'D; CLEANED AND PREPPED FOR CORE BOND; BONDED CORE; CLEANED AND PREPPED DOUBLER FOR BOND. FABRICATED AND BONDED DOUBLER, SEALED DOUBLER EDGE BJul 21, 2008 · N372FE · Doug MD1010FSDR SWAA084029Skin · delaminatedDURING SCHEDULED BRDG CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.Jul 21, 2008 · N513SW · Boeing 7375H4SDR SWAA084030Skin · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT UPPER SURFACE RT SIDE. REPAIRED FLAP PER SRM.Jul 21, 2008 · N513SW · Boeing 7375H4SDR UPS08552929Skin · dentedINSPECTION TYPE-C, RT IB MAIN FLAP UPPER SURFACE JUST OB OF AFT FLAP HAS MULTIPLE SMALL DENTS. MEASURED ALL DENTS ON RT IB FLAP UPPER SURFACE IAW SRM 57-53-01- 1A, DETAIL VII, FOUND (1EA) DENT AT GRID LOCATION "J5" TO BE OUT OF LIMITS. MEASUREMENT FOR THE DJul 20, 2008 · N430UP · Boeing 75724APFSDR SWAA084071Skin · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. R&R FLAP PER MM.Jul 20, 2008 · N674AA · Boeing 7373A4SDR SWIA200819896Attach Bracket · brokenLT NACELLE FLAP HAS A CRACKED ATTACH BRACKET. (FLIGHT NR 5480) REPLACED THE LT NACELLE FLAP IAW 27-50-03. Jul 19, 2008 · N295UX · Emb EMB120ERSDR USAA920081417Skin · delaminatedCLT- MAJOR REPAIR-C1 CHECK - RT WING INBOARD FOREFLAP UPPER RT SURFACE IS DELAMINATED. REPLACED RT WING INBOARD FOREFLAP IAW B737 AMM 27-51-07. (A)Jul 18, 2008 · N451UW · Boeing 7374B7SDR ASAA0843267Skin · dentedRT IB FOREFLAP LOWER SURFACE HAS A DENT ON IB END REMOVED DAMAGE FABBED FILLER & DOUBLER, BONDED IAW SRM 51-70-10 REPAIRS.Jul 18, 2008 · N755AS · Boeing 7374Q8SDR ASAA0843376Wedge · dentedRIGHT I/B MID FLAP LOWER SURFACE OF TRAILING EDGE WEDGE DENTED JUST O/B OF NR 3 TRACK. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10.Jul 17, 2008 · N754AS · Boeing 7374Q8SDR ASAA0843366Skin · dentedLT WING TRAILING EDGE I/B FORE FLAP SEVERAL DENTS ON LOWER SURFACE CENTER I/B AREAS. REMOVED DAMAGED DOUBLERS AND SKINS, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10.Jul 17, 2008 · N754AS · Boeing 7374Q8SDR ASAA0843354Skin · dentedLT WING O/B TRAILING EDGE AFT FLAP 3 EACH DENTS ON LOWER SURFACE. PREPARED DAMAGED AREAS, FABRICATED DOUBLERS AND BONDED IN ACCORDANCE WITH B737 400 SRM 51 70 10 REPAIR 2.Jul 17, 2008 · N754AS · Boeing 7374Q8SDR ASAA0843351Skin · dentedRT WING I/B TRAILING EDGE FOREFLAP HAS MULTIPLE DENTS ON LOWER SURFACE I/B AREA. PREPARED DAMAGED AREA, APPLIED ADHESIVE FILLER, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.Jul 17, 2008 · N754AS · Boeing 7374Q8SDR ASAA0843357Skin · chafedLT WING NR 3 L/E SLAT I/B LWR SURFACE OF T/E WEDGE CHAFED. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.Jul 17, 2008 · N754AS · Boeing 7374Q8SDR 08FDEA02960Panel · dentedLEFT WING OUTBD FLAP PANEL 535 AR HAS SEVERAL DENTS. REPAIRED DENTS IN THE LT WING OUTBD PANEL 535 AR WITH REPAIR DOUBLERS IAW SRM 51-71-00; VOL II.Jul 17, 2008 · N372FE · Doug MD1010FSDR 08FDEA02965Skin · delaminatedRT WING, INBD FLAP TRAIL EDGE UPPER AND LOWER SURFACE DELAMINATED AT 15.0 INCH FROM INBD EDGE, MEASURING 5.0 BY 2.0 INCH REPAIRED THE DELAMINATED WEDGE PER EA NR 6-5720-117366.Jul 17, 2008 · N456FE · Airbus A310222SDR SWAA084041Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. R&R FLAP PER MM.Jul 17, 2008 · N640SW · Boeing 7373H4SDR SWAA084040Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. R&R FLAP PER MM.Jul 17, 2008 · N640SW · Boeing 7373H4SDR 08FDEA02952Skin · damagedDURING ACCOMPLISHMENT OF EO 6-5750-7-5000 PT.3 FOUND DAMAGED HOLE ON LT INBOARD FLAP TOP SKIN NEAR RIB 7. REPAIR PERFORMED BY REAM UP THE HOLE TO DIAMETER 0.1865 -0.1895 INCH , INSPECT THE HOLE BY NDT AND INSTALL HL11VF-6 IAW RAS /FOK/165/2008 ISS.A, APPROVEDJul 17, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA02937Skin · damagedRIGHT WING INBD FLAP T/E LOWER SURFACE SKIN HAS LIGHTNING STRIKE DAMAGE 4 FEET FROM THE OUTBD EDGE. REPLACED SKIN P/N ARC 2736-4. THIS WAS ACCOMPLISHED ON N/R N00285, FOR DETAILS SEE SDR TRACKING NUMBER 08-3079.Jul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02933Skin · dentedRIGHT WING OUTBD FLAP LOWER SURFACE, OUTBD EDGE AREA SKIN HAS 6 EA DENTS. CHECKED DENTS AND FOUND THEM TO BE OUT OF LIMITS IN 2 PLACES FROM STA XOFH 773 - 778, IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT DAMAGED AREAS. MATERIAL ID FOR THE DOUBLER IS 2Jul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02935Skin · dentedRIGHT WING OUTBD FLAP LOWER SURFACE SKIN HAS A DENT 29 INCH OUTBD OF THE SPRING CARTRIDGE. CHECKED THE DENT AND FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT THE DAMAGED AREA. MATERIAL ID FOR THE DOUBLER IS 2024-T3, 0.050, Jul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02934Skin · dentedRIGHT WNG OUTBD FLAP LOWER SURFACE SKIN HAS A DENT, 1 FOOT OUTBD OF THE SPRING CARTRIDGE. CHECKED THE DENT AND FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT THE DAMAGED AREA. MATERIAL ID FOR THE DOUBLER IS 2024-T3, 0.050, PJul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02932Skin · dentedRIGHT WING INBD LOWER SURFACE SKIN HAS MULTIPLE DENTS JUST INBD OF THE OUTBD HINGE. CHECKED DENTS AND FOUND 2 OUT OF LIMITS IAW SRM 57-10-00, VOL I, FIG 48 AT STA XIFH 250 AND XIFH 254. REMOVED DAMAGED AREAS AND FABRICATED 2 REPAIR DOUBLERS IAW SRM 57-10-00,Jul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02936Skin · dentedRIGHT WING OUTBD FLAP SURFACE SKIN HAS 6 DENTS IN THE INBD EDGE AREA. CHECKED DENTS AND FOUND TO BE OUT OF LIMITS AT STA XOFH 478 AND 503 IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT DAMAGED AREAS. MATERIAL ID FOR DOUBLERS 2024-T3, 0.050, PO 623403.1,Jul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02931Skin · dentedLEFT WING INBD FLAP LOWER SURFACE HAS DENTS. CHECKED DENT AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I, FIG 48. REMOVED DAMAGE AND FABRICATED A REPAIR DOUBLER IAW DC/MD-10 SRM 57-10-00, VOL I, FIG 85. ALODINED AND PRIMED REPAIR DOUBLER IAWJul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02930Skin · chafedLEFT WING INBD FLAP LOWER SKIN IS DENTED. CHECKED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00; VOL I, FIG 48. REMOVED DAMAGE AND FABRICATED A REPAIR DOUBLER IAW SRM 57-10-00, VOL I, FIG 85. ALODINED AND PRIMED REPAIR DOUBLER IAW SRM 51-21-01, VOL IIJul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02929Skin · damagedLEFT WING OUTBD FLAP, INBD LOWER SKIN HAS TWO CREASES BETWEEN RIBS 3 AND 4 FROM THE INBD SIDE. REMOVED DAMAGED AREA IAW SRM 57-10-00, VOL I, FIG 85. FABRICATED A REPAIR DOUBLER IAW SRM 57-10-00, VOL I, FIG 85. ALODINE AND PRIMED REPAIR DOUBLER IAW SRM 51-21Jul 16, 2008 · N372FE · Doug MD1010FSDR 08FDEA02922Skin · crackedLEFT WING INBD AFT FLAP, 3RD ATTACH FITTING OUTBD SKIN CRACKED FABRICATED REPAIR PARTS AT LEFT WING T/E AFT FLAP, THIRD ATTACH FITTING O/B SKIN, REF 27-50-4 FIG 11. TREATED, PRIMED AND INSTALLED, REF SRM 51-20-2 PG 1-7, 57-50-04 FIG 11, 51-30-2 PG 2-4. PAIJul 16, 2008 · N273FE · Boeing 727233SDR 08FDEA02908Skin · chafedFOUND CHAFING MARKS ON LT INBOARD FLAP TOP SKIN RIB 1C. REPAIR PERFORMED BY INSTALLING EXTERNAL PATCH IAW RAS/FOK/161/2008 ISS B, APPROVED BY EA-5752-120086A.Jul 16, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA02885Skin · damagedLT WING T/E O/B FOREFLAP HAS DEEP GOUGE ON UPPER SURFACE AT WS 450. REMOVED DAMAGED AREA IAW B727 SRM 51-40-20 PARAGRAPH 12 AND FABRICATED FILLER AND DOUBLER FROM 2024T3 .016 (3 BY 3) AREA IAW B727 SRM 51-40-20 GAUGE 59. BONDED FILLER AND DOUBLER, SEALED EDGJul 15, 2008 · N275FE · Boeing 727233SDR SWAA083947Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.Jul 15, 2008 · N336SW · Boeing 7373H4SDR 08FDEA02853Support · crackedDURING OPEN-HOLE HFEC INSPECTION, CRACK INDICATION FOUND AT OUTBOARD LOWER FASTENER HOLE COMMON TO ARC4008 AND ARC4009 SUPPORTS OF LEFT HAND SIDE WING OUTBOARD FLAP. LEFT HAND OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRJul 14, 2008 · N597FE · Doug MD11FSDR 08FDEA02861Retainer · crackedLT WING TE FLAP WELL LWR PNL BULB SEAL RETAINER IS CRACKED 15 INCHES OUTBOARD OF NR 2 FLAP TRANSMISSION (MKD). REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED RETAINER REF DWG 65-21658 AND GMM 7-0-1001. INSTALLED SEAL RETAINER REF SRM 51-30-2 AND IDENTIFIJul 14, 2008 · N467FE · Boeing 727225SDR ASAA0843201Skin · dentedRT WING T/E AFT OB FLAP, 3 EACH DENTS CLOSE TOGETHER 5 TO 2 INCHES FROM T/E AND 21 INCHES FROM IB END. PREPARED DAMAGED AREA FABRICATED REPAIR DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2.Jul 12, 2008 · N797AS · Boeing 737490SDR CHQA200800138Bracket · unsecureFLIGHT 5586, RDU TO CLE. UPON FLAP RETRACTION FROM FLAPS 20 TO FLAPS 8 THE CREW RECEIVED A FLAP FAIL MESSAGE. THE MESSAGE WAS CONFIRMED AND THE LT FLAP WAS AT 11 DEGREES WHILE THE RT FLAP WAS AT 10 DEGREES. THE QRH CHECKLIST WAS FOLLOWED AND THE AIRCRAFT LAJul 11, 2008 · N701BR · Cndair CL6002B19SDR SWAA083905Skin · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.Jul 10, 2008 · N656SW · Boeing 7373H4SDR 08FDEA02978Fitting · corrodedRT WING, INTERIOR FITTING AT FRONT CARRIAGE NR 3 FLAP TRACK WITH CORROSION, DETECTED ON ACCOMPLISHMENT OF NR 0599. A NEW FITTING WAS FABRICATED SO AS TO REPLACE THE EXISTING ONE.Jul 10, 2008 · N721FD · Airbus A300B4622RSDR 2008UALA03813Skin · damagedRIGHT INBOARD MID AND AFT T/E FLAP HAS DAMAGE TO LOWER SURFACE. ALSO LOWER WING PANEL (652CB) WAS PUNCTURED AND HAS INTERIM REPAIR ACCOMPLISHED.Jul 10, 2008 · N644UA · Boeing 767322SDR 08FDEA02802Skin · damagedFOUND OLD FLUSH DOUBLER RPAIR ON RT CENTER FLAP NOSE SKIN WITHOUT ANY OLD DOCUMENTATION. REPAIR RENEWED IAW SRM 57-50-00 FIG 208.Jul 10, 2008 · N743FD · Airbus A300F4622RSDR CA080709004Carriage · grooved(CAN) LT INBD FLAP MAIN 1 CARRIAGE ASSY (P/N 190-92001-405) FOUND GROOVED INSIDE BY LOOSE BOLT FROM TRACK ASSY. ENGINEERING ADVISED THE ROOT CAUSE OF THE DAMAGE OF THE FLAP CARRIAGE IS CAUSE BY THE FLAP TRACK MECHANISM LOOSE BOLT.Jul 9, 2008 · Emb ERJ190100IGWSDR SWAA083814Flap · debondedDURING SCHEDULED SPV CHECK, FOUND LH WING INBOARD FORE FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.Jul 9, 2008 · N378SW · Boeing 7373H4SDR SWAA083811Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Jul 9, 2008 · N355SW · Boeing 7373H4SDR 08FDEA02759Skin · gougedDEEP GOUGE IN LT O/B FOREFLAP, L/E CAP UPPER SURFACE APPROX 10 INCHES FROM I/B END IN PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1' X 5/8 IAW B727 SRM 57-50-4 FIG 1. FABRICATED REPAIR PLATE MAT USED 2024T3 .063' Jul 8, 2008 · N275FE · Boeing 727200SDR 08FDEA02742Skin · damagedFOUND OLD DOUBLER REPAIR ON LT INNER FLAP UPPER SKIN NEAR RIB 27, STRG 2.1 AND 2.2 WITHOUT AI APPROVAL. DOUBLER REPAIR RENEWED IAW RAS/FOK/198/2008 ISS A, APPROVED EA 6-5752-123008.Jul 8, 2008 · N742FD · Airbus A300B4622RSDR 08FDEA02718Strap · crackedLEFT WING OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP FOUND CRACKED. LEFT WING OUTBOARD FLAP INBOARD FLAP HINGE TENSION STRAP REMOVED AND REPLACED AS PER FEDEX EO NR 1-5750-7-5004 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 6, 2008 · N601FE · Doug MD11FSDR WRL2008F00004Rib · crackedDURING 1C + 12A CHECK FOUND STOP RIB CRACKED AT RT OB FLAP. IAW DOCUMENT NR 08-57-57 SECTION 1, ADJUST RT OB FLAP NR 2 UP STOP BOLT IN THE RIB. COND CHECK NORMAL. (K)Jul 6, 2008 · N274WA · Doug MD11FSDR WRL2008F00001Rib · crackedDURING 4C + 12A, CHECK FOUND STOP RIB CRACKED AT LT OB FLAP. IAW DOCUMENT NR 08-57-56 SEC 1, ADJUST LT OB FLAP NR 2 UP STOP BOLT IN THE RIB COND CHK NORMAL. (K)Jul 6, 2008 · N274WA · Doug MD11FSDR IXX2008F00108Skin · brokenDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING OTBD FLAP UPPER SKIN BROKEN AT STA XF 169.000-213.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED Jul 5, 2008 · N830BX · Doug DC871FSDR 08FDEA02715Skin · crackedRT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED RT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKED. STOP DRILLED CRACK DIMS .250 IAW SRM 51-10-1. HFEC INSPECTED STOP DRILL IAW NDTM PT 6 51-00-00 FIG 23 CRACK TERMINATES IN STOP DRILL HOJul 5, 2008 · N494FE · Boeing 727227SDR 08FDEA02714Skin · crackedLT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED LT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKED. STOP DRILLED CRACK IAW SRM 51-10-1 DIMS .250. HFEC INSPECTED STOP DRILL IAW NDTM 51-00-00-FIG 23 CRACK TERMINATES IN STOP DRILL HOLE. Jul 5, 2008 · N494FE · Boeing 727227
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