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 FDEA201009273737Skin · debondedFLAP OTBD RT - LOWER SKIN SURFACE BTW RIB7 AND RIB 9 FOUND DEBONDED. FLAP OUTBOARD DISBONDED AREA WAS REPAIR IAW EA 6-5750-144062.Sep 27, 2010 · N456FE · Airbus A310222SDR REXA201000163Seal · missingLEFT WING OUTBOARD FLAP OUTBOARD HINGE FAIRING SEAL WAS FOUND MISSING. TEMPORARY REPAIR IAW STS EA 5-2010-187; FILLED THE MISSING SEAL AREA IAW SRM 51-23-00 EXCEPT USED RTV 157. APPLIED SPEED TAPE PER SRM 51-27-15 OVER THE SEALANT TO PROTECT THE MATERIAL FROSep 27, 2010 · N8794B · Cndair CL6002B19SDR SWAA105784Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.Sep 27, 2010 · N606SW · Boeing 7373H4SDR COMA2010092850209Vane · chafedRIGHT I/B FLAP VANE LEADING EDGE FOUND TO HAVE CHAFE DAMAGE. REPLACED THE RIGHT I/B FLAP VANE LEADING EDGE IAW CRJ 200 SRM.Sep 27, 2010 · N965CA · Cndair CL6002B19SDR DALA1023925809Panel · puncturedDURING L-CHECK FOUND PUNCTURE IN LOWER SURFACE OF RT WING INBD MAIN FLAP T/E PANEL. REPAIRED IAW SRM 51-70-17 PARA 4, AMM 51-21-10-377-003, TABLE 701.Sep 27, 2010 · N588NW · Boeing 757351SDR FDEA201009273735Skin · chafedRT WING CTR FLAP UPPER SURFACE APPROX WING RIB 13 (2EA) WEAR MARKS FROM BUTTON HEAD RIVETS REPAIRED RT CTR FLAP UPPER SKIN IAW SRM 57-50-00, FIG 205 USING DOUBLER REPAIR SCHEME.Sep 27, 2010 · N745FD · Airbus A300B4622RSDR FDEA201009273733Skin · chafedLT WING T/E FLAP AT RIB 13 UPPER SURFACE HAS 6 EA CHAFE MARKS. REPAIRED LT CTR FLAP UPPER SKIN IAW SRM 57-50-00, FIG 205, DOUBLER REPAIR METHOD.Sep 27, 2010 · N745FD · Airbus A300B4622RSDR DALA1023999886Attach Bracket · crackedDURING H-CHECK, FOUND CRACK IN RT WING FLAP ATTACH BRACKET INSIDE OF ACCESS HOLE RIB INBD OF NR4 HINGE. REPAIRED IAW SRM 51-30-2, SRM 51-10-4 & SRM 51-30-2, PAGE 205.Sep 26, 2010 · N600TR · Doug DC951SDR UIEA2010092600163Fairing · damagedDURING WALK-AROUND INSPECTION, MX REPORTED THE NR 8 FLAP TRACK FAIRING 'CANOE' DAMAGED WITH A CRACK AND 2 DENTS (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, DVI INSPECTIONS AFTER EVERY 5 FLIGHT Sep 26, 2010 · N492MC · Boeing 74747UFSDR USAA2010093092161Flap Track · corrodedCLT - Q6 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 8 FLAP TRACK TRANSMISSION MOUNT HOLE. REPLACED NR 8 FLAP TRACK IAW B737 AMM 27-51-49.Sep 24, 2010 · N532AU · Boeing 7373B7SDR DALA1024239868Vane · gougedDURING M-CHECK FOUND GOUGE IN LT WING INBD FIXED VANE L/E. REPAIRED IAW SRM 51-70-2, SRM 05-10-02 PAGE 226.Sep 24, 2010 · N777NC · Doug DC951SDR DALA1024019886Vane · dentedDURING H-CHECK FOUND SEVERAL SMALL DENTS IN LT WING INBD FIXED VANE. REPAIRED IAW SRM 51-70-2.Sep 24, 2010 · N600TR · Doug DC951SDR DALA1024009886Vane · brokenDURING H-CHECK FOUND LT WING INBD FIXED VANE T/E BROKEN AND DEBONDED. REPAIRED IAW SRM 51-70-2.Sep 24, 2010 · N600TR · Doug DC951SDR FDEA201009233778Wedge · corrodedRT OTBD FLAP SEC WEDGE PANEL, INBD TOP SKIN REQUIRES REPLACEMENT BECAUSE OF CORROSION. REPAIRED SKIN IAW SRM 57-10-00, FIG 7, VOL I AND SRM 51-31-01, VOL II. FABRICATED 1 EA DOUBLER IAW DWG ARC 1953, REV "J". FABRICATED -34 AND -35 TEE CAPS IAW DWG ARC 1953Sep 23, 2010 · N370FE · Doug MD1010FSDR FDEA201009233665Skin · wornRT OTBD FLAP UPPER SKIN HAS SEVERAL WORKING FASTENERS AND 1 MISSING FASTENER AFT OF THE INBD FLAP HINGE FITING ALONG THE T/E. REMOVED WORKING FASTENERS IAW SRM 57-20-00, FIG 11, VOL I. FABRICATED BEARING STRAPS, APPLIED ALODINE AND PRIMER IAW SRM 51-21-01, Sep 23, 2010 · N389FE · Doug MD1010FSDR IPXA10662787Skin · damagedON ARRIVAL FOUND DAMAGE TO OTBD FLAP L/E SKIN PANEL 666FT, 3.5"X0.75" LOCATED 1.5" FROM L/E OF PANEL AND 1.5" FROM OTBD EDGE OF PANEL. REPAIRED IAW SRM 57-53-01-2R FIG 201 AND SRM 51-70-03.Sep 23, 2010 · N324UP · Boeing 76734AFSDR DALA1023719886Vane · chafedDURING M-CHECK FOUND RT WING INBD FIXED VANE CHAFED ON INBD AND OTBD ENDS. REPAIRED IAW SRM 57-50-9 &1-70-02.Sep 23, 2010 · N600TR · Doug DC951SDR IPXA10663010Wedge · puncturedINSPECTION TYPE:C, RT WING OTBD FLAP UPPER SURFACE T/E WEDGE PUNCH HOLE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 48.Sep 22, 2010 · N305UP · Boeing 76734AFSDR IPXA10662988Skin · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP LWR SURFACE INBD AFT PANEL INBD AREA FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 48.Sep 22, 2010 · N305UP · Boeing 76734AFSDR IPXA10662964Wedge · puncturedINSPECTION TYPE:C, RT WING OTBD FLAP T/E WEDGE UPPER SURFACE PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 48.Sep 22, 2010 · N305UP · Boeing 76734AFSDR FDEA201009223651Skin · wornRIGHT OUTBD FLAP UPPER SKIN HAS SEVERAL WORKING FASTENERS AFT OF THE INBD FLAP HINGE FITTING. REMOVED WORKING FASTENERS IAW SRM 57-20-00, FIG 11, VOL I. FABRICATED BEARING STRAPS, MATERIAL ID 2024-T3 0.050 IAW SRM 57-20-00, FIG 11, VOL I. APPLIED ALODINSep 22, 2010 · N389FE · Doug MD1010FSDR SWAA105769Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.Sep 22, 2010 · N692SW · Boeing 7373T5SDR FDEA201009223616Skin · dentedLT WING INBD LOWER FLAP LOWER SKIN IS DENTED 5" FROM THE T/E FROM WS XIFH 296 TO WS XIFH 300. REMOVED DAMAGED AREA; FABRICATED DOUBLER AND FILLER IAW SRM 57-00-01, FIG 4, SHEET 2, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. PAINTED IAW SRM 51-21-0Sep 22, 2010 · N389FE · Doug MD1010FSDR FDEA201009223650Skin · looseRIGHT OUTBD FLAP UPPER SKIN HAS SEVERAL WORKING FASTENERS JUST IND OF THE NR 2 FLAP TRACK CENTER AREA. REMOVED WORKING FASTENERS IAW SRM 51-35-20, VOL II. FABRICATED 5 EA REPAIR DOUBLER STRIPS. ALODINED TREATED AND PRIMED IAW SRM 51-21-01, VOL II. INSTASep 22, 2010 · N389FE · Doug MD1010FSDR USAA2010092292071Skin · crackedMAJOR REPAIR - CRACK ON LT WING OTBD MID FLAP L/E SKIN BETWEEN WBL204.4 TO WBL219.4. REPAIRED LT WING OTBD MID FLAP L/E SKIN BETWEEN WBL204.4 TO WBL219.4 IAW SRM 57-53-01 REPAIR NR 8.Sep 22, 2010 · N334AW · Boeing 7373Y0SDR IPXA10662963Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-71-05, PAR 5A(1) FIG 5, REV 48.Sep 21, 2010 · N305UP · Boeing 76734AFSDR IPXA10662962Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 48.Sep 21, 2010 · N305UP · Boeing 76734AFSDR REXA201000153Hinge · damagedDAMAGE WAS FOUND ON THE RIGHT WING INBOARD FLAP HINGE ARM ASSEMBLY ON THE UPPER SURFACE OF THE INBOARD LUG AT WS=127. DAMAGE TO THE P/N 601R10917-2 HINGE ARM ASSEMBLY CONSISTS OF A GOUGE MEASURING 0.020 INCH LONG BY 0.090 INCH WIDE WITH A MAXIMUM DEPTH OF 0.0Sep 21, 2010 · N8877A · Cndair CL6002B19SDR DALA1023549860Skin Panel · dentedDURING GROUND INSP FOUND DENT IN LT INBD FLAP OTBD SKIN PANEL JUST AFT OF L/E. REPLACED IAW DWG 5910134.Sep 21, 2010 · N769NC · Doug DC951SDR DALA1023539860Access Panel · damagedDURING GROUND INSP FOUND DAMAGE TO LT INBD FLAP ACCESS PANEL. REPLACED IAW SRM 53-00-00.Sep 21, 2010 · N769NC · Doug DC951SDR DALA1023519860Wedge · damagedDURING GROUND INSP, FOUND DAMAGE TO LT FLAP T/E WEDGE OTBD OF AFT INBD SPOILER. REPAIRED IAW SRM 57-03-10.Sep 21, 2010 · N769NC · Doug DC951SDR IPXA10M62684Skin · damagedRT WING INBD FLAP OTBD LWR SKIN DAMAGED. REPAIRED IAW EO MD11-5750-39705-A.Sep 20, 2010 · N291UP · Doug MD11FSDR SWAA105597Skin · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER MM.Sep 20, 2010 · N310SW · Boeing 7373H4SDR FDEA201009173522Wedge · corrodedRIGHT OUTBD FLAP, NR 2 WEDGE LOWER SKIN AND FINGER DOUBLER IS CORRODED AND DISBONDED. REPAIRED SKIN IAW SRM 57-10-00, FIG 7, VOL I AND SRM 51-31-01, VOL II.Sep 17, 2010 · N370FE · Doug MD1010FSDR IPXA10M62868Skin · dentedINSPECTION TYPE:2C, LT WING INBD FLAP UPPER SKIN SURFACE IS DENTED, CREASED REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOULBER IAW SRM 57-00-01, REPAIR 1, FIG 201.Sep 17, 2010 · N273UP · Doug MD11FSDR REXA201000150Fairing · chafedRT WING FLAP STUB FAIRING ASSEMBLY (P/N 601R31199) WAS FOUND WITH CHAFE DAMAGE. THE DAMAGE IS THE RESULT OF A FASTENER / PACKER THAT SECURES THE P/N 601R14016 SEAL TO THE INBOARD FLAP PROTRUDING AND CONTACTING THE STUB FAIRING DURING NORMAL FLAP MOVEMENT. CHSep 17, 2010 · N8698A · Cndair CL6002B19SDR UALA2010092103511Skin · dentedLEFT WING INBD T/E AFT FLAP LOWER SURFACE HAS NUMEROUS DENTS.Sep 17, 2010 · N654UA · Boeing 767322SDR FDEA201009173534Skin · damagedLEFT WING OTBD FLAP LOWER SKIN DISBONDED 7.5 IN LENGTH X 1.5 IN WIDE AT T/E,48 IN INBD FROM OTBD EDGE. REPAIRED LT WING T/E SKIN IAW EA 6-5750-135278 - WINGS - LT OTBD FLAP T/E -REPAIR TRACKING EA.Sep 17, 2010 · N425FE · Airbus A310203SDR UALA2010092003473Skin · dentedLT WING INBD T/E AFT FLAP LOWER SURFACE HAS NUMEROUS DENTS. NUMEROUS DENTS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY OF EACH OTHER IAW SRM. REMOVED AFT FLAP AND MRO PROVIDER SENT FLAP OUT FOR REPAIR. FLAP REPAIRED IAW AES-10-082 AND EA PD67-57-011 AND INSTALLSep 17, 2010 · N654UA · Boeing 767322SDR FDEA201009153656Skin · misrepairedFLAP INBD LT LOWER SKIN - PREVIOUS REPAIR FOUND BETWEEN RIB13/14 AND STGR 8/11. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO THE SRM. NEW REPAIR ACCOMPLISHED IAW EA 6-5750-144069 INSTRUCTIONS.Sep 15, 2010 · N456FE · Airbus A310222SDR IXXA10SMN082SSkin · wornDURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP UPPER EXTERNAL SKIN WORN AT STA XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDSep 15, 2010 · N606AL · Doug DC873FSDR IXXA10SMN081SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND LT WING INBD FLAP UPPER EXTERNAL SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEWSep 15, 2010 · N606AL · Doug DC873FSDR IXXA10SMN080SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP LOWER EXTERNAL SKIN CRACKED AT STATION XCW 64.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATSep 15, 2010 · N606AL · Doug DC873FSDR IXXA10SMN078SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT OTBD FLAP UPPER SKIN CORRODED AT STATION XF 304.000 - 333.0000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDSep 15, 2010 · N606AL · Doug DC873FSDR A6WA201040699Flap Track · wornLT OTBD FLAP OTBD VANE TRUCK IS NEARLY FLUSH WITH VANE SKIN. REQUIRES BUTTE DOOR RIGGING AFTER REPAIR. R & R LT OTBD FLAP VANE OTBD TRACK PN 601R14502-1, IAW REO 601R-57-53-016.Sep 15, 2010 · N407AW · Cndair CL6002B19SDR FDEA201009153533Skin · corrodedLT OTBD MAIN FLAP CORRODED ON LOWER SURFACE AT WS 409 AND WS 429. CUT OUT DAMAGED AREA OF CHORD DIMS 33" IAW SRM 51-70-12. FABRICATED 2 ANGLES, 1 ANGLE, HEAT TREATED ANGLES TO 2024T-3 IAW FAS ENG REPORT NR 2-37153-801, REV A FABRICATED CHORD AND 1 RADIUS FILLSep 15, 2010 · N918FD · Boeing 75723ASDR UALA2010091603447Skin · damagedLEFT T/E OTBD FLAP DAMAGED. 2 "L"SHAPED HOLES MEASURE 1IN BY 1 IN AND .5 BY .5IN. OVERALL LENGTH EQUALS 2.5 IN BY 1 IN. DAMAGE IS LOCATED UNDER SIDE OF FLAP, 18 IN UP FROM T/E, AND 30 IN. IN FROM INBD EDGE OF FLAP. FOUND DELAMINATION BETWEEN BOTH HOLES AND ASep 15, 2010 · N773UA · Boeing 777222SDR UALA2010091603441Support Fitting · damagedTHE NR 5 FLAP TRACK FWD SUPPORT FITTING HAS SEVERAL TOOL MARKS IN THE OTBD WEB AREA. (DAMAGE IS MARKED IN RED) BLENDED FITTING. TREATED AND PRIMED BLENDED AREA. IAW EVA 80076 NEED TO ACCOMPLISH CATEGORY B ROTO PEEN AT NEXT SCHEDULED D4 CHECK OCT 29 2012. MF64Sep 15, 2010 · N180UA · Boeing 747422SDR UALA2010091603440Support Fitting · gougedTHE NR 4 FLAP TRACK FWD SUPPORT FITTING HAS GOUGE IN THE OTBD WEB AREA. (DAMAGE IS MARKED IN RED). BLENDED FITTING IAW SRM. TREATED AND PRIMED BLENDED AREA. IAW EVA 80076 NEED TO ACCOMPLISH CATEGORY B ROTO PEEN AT NEXT SCHEDULED D4 CHECK OCT 29 2012. MF6450 Sep 15, 2010 · N180UA · Boeing 747422SDR SWAA105577Flap · damagedDURING SCHEDULED MV1 CHECK, FOUND LT WING AFT O/B FLAP DAMAGED. REMOVED AND REPLACED AFT FLAP PER MM.Sep 15, 2010 · N945WN · Boeing 7377H4
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