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"

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 08FDEA02145Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 3 AND NR 4, MEASURING 3.9 IN BY 13.8 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKIN REPAIR ON LT WJun 4, 2008 · N443FE · Airbus A310203SDR 08FDEA02146Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP UPPER MAIN RUB STRIP BETWEEN RIB 4 AND RIB 5, MEASURING 6.9 IN BY 13.0 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKIN REPAIR ON LT WING OUTBD FJun 4, 2008 · N443FE · Airbus A310203SDR 08FDEA02159Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP UPPER SKIN UNDER RUB STRIP BETWEEN RIB NR 3 AND RIB NR 4 AND 3.6 IN FWD OF REAR SPAR MEASURING 4.4 IN BY 14.2 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTEJun 4, 2008 · N443FE · Airbus A310203SDR 08FDEA02158Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 2 AND RIB NR 3 AND 9.6 IN FWD OF REAR SPAR MEASURING 7.5 IN BY 7.1 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT Jun 4, 2008 · N443FE · Airbus A310203SDR 08FDEA02157Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 6 AND RIB NR 7, MEASURING 3.9 IN BY 4.1 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKIN REPAIR ON RT WINJun 4, 2008 · N443FE · Airbus A310203SDR 08FDEA02155Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBD FLAP UPPER SKIN UNDER RUB STRIP BETWEEN RIB NR 3 AND RIB NR 4, MEASURING 4.1 IN BY 11.9 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKIN REPAIR ON RT WING Jun 4, 2008 · N443FE · Airbus A310203SDR 2008UALA03170Spar · damagedFOUND RT MID FLAP L/E SPAR DAMAGED. FOUND RT MID FLAP L/E SPAR DAMAGED. CONNECTING LINKAGE FOR EXHAUST GATE CAME LOOSE AND DAMAGED CUTOUT SECTION THAT ROD GOES THROUGH. REMOVED FLAP. INSTALLED NEW MID FLAP. FLAP ASSY INSTALLED. TEST FLT OKAY. Jun 3, 2008 · N312UA · Boeing 737322SDR 08FDEA02134Angle · crackedRT WING INBOARD MID FLAP LOWER AFT CHORD ANGLE IS CRACKED AT WBL 110. CUT OUT DAMAGED SECTION DIM 47 1/4 INCH IAW B727 SRM 51-10-1, FABRICATED FILLER REPAIR USING BAC1503-100046 7075-T6 PO NR 8177105 DIM 47 1/4 INCH BY 2 INCH AND SPLICE USING BAC1503-100046 7Jun 3, 2008 · N274FE · Boeing 727233SDR 08FDEA02136Skin · delaminatedLT WING O/B FLAP I/B END BY END FITTING IS DELAMED (TOP SKIN ) OF FORE FLAP REPAIRED LT WING OUTBOARD FORE FLAP REF SRM 51-40-20 PAR'S 7,14,15,18,20,21 PGS 12-62 SRM 57-50-02 FIG 4 PG 7, AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Jun 3, 2008 · N487FE · Boeing 727227SDR 08FDEA02091Angle · wornLEFT WING LOWER TRAILING EDGE OUTBD FLAP; AT THE OUTBD SIDE OF THE HINGE FAIRING (XORS 500) ANGLE IS FRETTING FROM CONTACT WITH THE INBD SIDE OF PANEL NR 551 BB. CHECKED ANGLE AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; VOL I; FIG 1- A. ORIGINJun 2, 2008 · N357FE · Doug MD1010FSDR 08FDEA02085Panel · wornRIGHT WING INBD FLAP HINGE PANEL 641 BR IS WORN. REPAIRED RIGHT WING INBD FLAP HINGE PANEL 641 BR BY REMOVING DAMAGED AREA AND BONDING A FILLER AND DOUBLER REPAIR IAW DC/MD-10 SRM 51-71-00; VOL II. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-2-01; VOL II AND SEAJun 2, 2008 · N357FE · Doug MD1010FSDR SWAA082918Flap Track · corrodedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 FLAP TRACK CORRODED AT AFT MOUNT PAD. REMOVED AND REPLACED FLAP TRACK PER MM.Jun 1, 2008 · N358SW · Boeing 7373H4SDR USAA920081228Skin · debondedMCN - C12 - MAJOR REPAIR - NR 6108532 - I/B TRAILING EDGE DISBONDED, RIGHT WING I/B AFT FLAP. REPAIRED I/B TRAILING EDGE RIGHT WING I/B AFT FLAP DISBONDED IAW SRM 51-70-04-0G. (K)May 31, 2008 · N905AW · Boeing 7572S7SDR USAA920081312Rivet · looseCLT - C22 - MAJOR REPAIR - LT OUTBOARD FOREFLAP HAS SEVERAL SMOKING RIVETS. REPLACED FOREFLAP IAW B737 AMM 27-51-37. (S)May 30, 2008 · N316AW · Boeing 7373S3SDR DLM88080801Vane · erodedDURING HMV3 ERODED LOWER SURFACE OF INBD FIXED VANE LT INBD FLAP WAS FOUND. EROSION WAS REPAIRED IAW SRM 57-03 PARA 8D FIG 9A.May 30, 2008 · N963DL · Doug MD88SDR USAA920081305Flap · delaminatedCLT - C22 - MAJOR REPAIR - RT WING INBOARD FOREFLAP HAS AREA OF DELAMINATION. REPLACED RT WING INBOARD FOREFLAP IAW B737 AMM 27-51-07. (S)May 29, 2008 · N316AW · Boeing 7373S3SDR 2008UALA03093Skin · dentedLEFT INBOARD FLAP DENT AND ABRASION ON TRAILING EDGE, CENTER AFT OF NR 2 TIRE. FOUND AND REPORTED BY RAMP DURING WALKAROUND. *S/D* IDENTIFIED BY SRM 57-50-00- 001 PG 7 INBOARD FLAP. DAMAGE AREA PER SRM 57-52-00-101 PG 4 AS ZONE 2, PER TABLE 101 PG 2. DENTMay 29, 2008 · N497UA · Airbus A320232SDR SWAA082906Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP UPPER INBOARD SURFACE DELAMINATED. REPAIRED FLAP PER SRM.May 29, 2008 · N634SW · Boeing 7373H4SDR SWAA082897Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP OUTBOARD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.May 29, 2008 · N399WN · Boeing 7373H4SDR SWAA082892Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP UPPER INBOARD SURFACE DELAMINATED. REPAIRED FLAP PER SRM.May 29, 2008 · N333SW · Boeing 7373H4SDR DHL2008764533Attach Angle · crackedWHILE AT C CHECK, LT O/B MID FLAP I/B LOWER END CAP AND ATTACHMENT ANGLE CRACKED. REPAIRED IAW B727 SRM 51-40-2, 51-20-1, 51-30-5 AND 57-50-2 FIG 6. REPAIR ANGLE MAT.7075 T6 .071" PO NR 9006522 DIM 4 INCH BY 4 INCH AND 3 INCH BY 2 INCH.May 29, 2008 · N764AT · Boeing 727264SDR COEA0810911Rib · corrodedFOUND DURING HEAVY CHECK AT COE. LEVEL 2 CORROSION ON RT WING OUTBOARD FLAP, FLAP RIB 18 FWD PICK UP IS EXFOLIATING INSIDE OF FLAP. REPLACED OUTBOARD FLAP ASSEMBLY. (S)May 28, 2008 · N911FX · Aerosp ATR42300SDR 2008UALA03039Skin · dentedRIGHT WING I/B MAIN FLAP UPPER SURFACE OUTBOARD SIDE ATTACHED SCREW HOLES HAVE 3 DENTS. SUSPECT TOOLING MARKS. ACP REPAIR PER AMECO 777EN -57-0045-01. THE REPAIR IS APPROVED BY BAC, AND 8100-9 THE REPAIR IS A PERMANENT REPAIR. AC OK FOR SERVICE.May 28, 2008 · N780UA · Boeing 777222SDR 2008UALA03038Skin · wornLEFT WING O/B FLAP UPPER SURFACE ARE WORN AT LOCATIONS: 1" TO 9", 62" TO 71", 147" TO 168", AND 220" TO 240". DAMAGED LOCATION IS MEASURED FROM I/B END. MAX DAMAGE DEPTH IS .080". SUSPECT NORMAL AC OPERATION. ACP REPAIR PER AMECO, 777E N-57-0041-01. THE RMay 28, 2008 · N780UA · Boeing 777222SDR 2008UALA03037Skin · crackedLEFT WING I/B TRAILING EDGE MAIN FLAP UPPER SURFACE HAS CRACK AT LOCATION AT 82 INCHES FROM I/B END. SUSPECT NORMAL AC OPERATION. ACP REPAIR PER AMECO 777EN -57-0044-01. THE REPAIR IS APPROVED BY BAC 8100-9 THE REPAIR IS A PERMANENT REPAIR. AC OK FOR SERVIMay 28, 2008 · N780UA · Boeing 777222SDR 2008UALA03036Skin · wornRIGHT O/B FLAP UPPER SURFACES ARE WORN. SUSPECT NORMAL AC OPERATION. ACP RPR FROM AMECO 777EN 57-0040-01. THE REPAIR IS APPROVED BY BAC 8100-9. THE REPAIR IS PERMANENT REPAIR. AC OK FOR SERVICE.May 28, 2008 · N780UA · Boeing 777222SDR 08FDEA02599Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON INBD FLAP RT, RIB 24B, LOWER AND TOP SKIN T/E. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPMay 27, 2008 · N721FD · Airbus A300B4622RSDR 2008UALA03030Fairing · damagedON WALK AROUND FOUND DAMAGE TO OUTBOARD SIDE OF OUTBOARD FLAP CANOE FAIRING ON INBOARD LEFT FLAP. DAMAGE APPROX 8 INCHES LONG BY 2 INCHES AT WIDEST POINT, ALSO TWO GRAZE MARKS BELOW DAMAGE 3 INCHES AND 4 INCHES LONG. ACCOMPLISHED PERMANENT REPAIR REF SRM 57May 26, 2008 · N179UA · Boeing 747422SDR ASAA0843008Skin · dentedRT OTBD AFT FLAP HAS A DENT 23 INCHES FROM INBD END ON UPPER SURFACE. REMOVED DAMAGED SKIN FABBED FILLER SKIN AND EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PARA'S 20 22 PGS 254 257.May 25, 2008 · N703AS · Boeing 737490SDR A6WA200840446Plate · gougedGOUGE FOUND ON AFT HINGE LOG PLATE OF LT INBOARD FLAP. GOUGE REMOVED IAW REO 601R-57-1343. (A)May 23, 2008 · N406AW · Cndair CL6002B19SDR A6WA200840445Plate · gougedGOUGE FOUND ON AFT HINGE LOG PLATE OF RT INBOARD FLAP. GOUGE ON AFT HINGE LUG PLATE OF RT INDB FLAP REMOVED IAW REO 601R-57-52-1341. (A)May 23, 2008 · N406AW · Cndair CL6002B19SDR A6WA200840444Attach Fitting · gougedLEFT OUTBOARD FLAP, OUTBOARD FLAP HINGE ARM FOUND GOUGED ON BEARING ATTACHMENT PLATE, FWD FACE. GOUGE ON BEARING ATTACHMENT PLATE FWD FACE REMOVED IAW REO 601R-57-54-112. (A)May 23, 2008 · N406AW · Cndair CL6002B19SDR 2008UALA02971Flap · damagedCRACK HAS MIGRATED THRU THE RT INBOARD T/E FLAP. ALSO HAVE DELAM ON BOTH SIDES OF CRACK. COMPOSITE DELAMINATION. ACP INTERIM REPAIR PER SRM 57-53-01, PERMANENT REPAIR ACCOMPLISHED PER EVA-71598.May 23, 2008 · N590UA · Boeing 757222SDR 2008UALA02974Flap · delaminatedLEFT WING AFT INBOARD FLAP OUTBOARD EDGE APPEARS TO BE DELAMINATED. SUSPECT MOISTURE CONTAMINATION. REPAIRED BY SHOP MECHANIC PER GNMM 01-0-01-024. AC OK FOR SERVICE.May 22, 2008 · N941UA · Boeing 737522SDR UPS08152418Skin · chafedINSPECTION TYPE:3C LEFT WING CENTER FLAP UPPER SKIN MID SECTION HAS 6 CHAFE MARKS. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00 FIG 206, 51-40-21 AND EO M-5100-19814-D.May 22, 2008 · N137UP · Airbus A300F4622RSDR DHL2008764518Flap · crackedLEFT INBOARD FORE FLAP CRACK INDICATIONS AT L/E FWD OF SEQUENCE CAR ATTACH POINTS (FITTING) WBL 124/203. STOP DRILLED AT THE END OF CRACKS AT LEFT INBOARD FORE FLAP L/E WBL 124/203 IAW B727 SRM 51-10-1. FAB DOUBLER REPAIR WITH 2024-T3 .050" AND PO 9006457 I/May 22, 2008 · N764AT · Boeing 727264SDR 08FDEA01948Skin · damagedFOUND OLD DOUBLER REPAIR ON RT INNER FLAP LOWER SKIN, RIB 1C-3 WITHOUT ANY OLD DOCUMENTATION AVAILABLE. REPAIR RENEWED (PATCH REPAIR) IAW RAS RAS/FOK/086/2008 ISS A, APPROVED BY EA 6-5752-120047.May 22, 2008 · N742FD · Airbus A300B4622RSDR 08FDEA01947Skin · damagedFOUND OLD REPAIR ON RT INNER FLAP UPPER SKIN, RIB 11-12 WITH NEW DAMAGES, (2 NICKS ON DOUBLER). REPAIR RENEWED IAW SRM 57-50-00 FIG 205.May 22, 2008 · N742FD · Airbus A300B4622RSDR UPS08852579Flap · damagedINSPECTION TYPE:C2 INTERIM REPAIR TO RT INBOARD FLAP AT TRAILING EDGE XM-75. REMOVED INTERIM REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-21A, 51-1-8, 51-1-9A.May 21, 2008 · N802UP · Doug DC873FSDR UPS08152417Skin · gougedINSPECTION TYPE:3C LEFT I/B FLAP UPPER SKIN MID SECTION 6 INCH LONG GOUGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00.May 21, 2008 · N137UP · Airbus A300F4622RSDR UPS08152416Skin · chafedINSPECTION TYPE:3C LEFT I/B FLAP UPPER L/E SKIN CHAFED 8 INCH HORIZONTALLY. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00.May 21, 2008 · N137UP · Airbus A300F4622RSDR DHL2008764514Flap · crackedL/WING I/B MIDFLAP T/E CHORD CRACKED AT I/B CABLE DRUM, 2 PLACES. REMOVED DAMAGED AREA AT T/E CHORD ABOUT 51 INCHES. FABRICATED NEW SECTION WITH P/N 604754 7075-T6 DIM 51 INCH AND PO 815986 IAW B727 SRM 57-50-2 FIG 5 AND 51-40-1 FIG 1.May 21, 2008 · N764AT · Boeing 727264SDR 08FDEA01946Fairing · crackedNR 4 T/E FLAP TRACK FWD FAIRING, HAS CRACK AT FWD END CUTOUT REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, NDT CHECKED FAIRING AND FOUND CRACK TO BE TERMINATED. MADE ADDITIONAL CUT FINALE CUT. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED. INSTALLEDMay 21, 2008 · N220FE · Boeing 727233SDR SWAA082772Wedge · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD MID FLAP WEDGE DELAMINATED AT INBOARD END. REMOVED AND REPLACED WEDGE PER MM.May 21, 2008 · N370SW · Boeing 7373H4SDR SWAA082756Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.May 21, 2008 · N302SW · Boeing 7373H4SDR 08FDEA01888Skin · dentedRT WING INBD FLAP LOWER SURFACE FOUND WITH 3 DENT MARKS AT XIFH 249. DENTS ON RIGHT HAND WING INBD FLAP LOWER SURFACE AT XIFH 249 MEASURED AND FOUND OUT OF LIMITS AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 3 VOLMay 20, 2008 · N590FE · Doug MD11FSDR ASAA0873021Skin · dentedRT WING INBD MAIN FLAP UPPER AFT ACCESS PANEL HAS DENT AT OTBD SIDE. RT WING INBD MAIN FLAP UPPER AFT ACCESS PANEL DENT REPAIRED IAW B737 700 SRM 51 70 10 REPAIR 2.May 20, 2008 · N613AS · Boeing 737790SDR DL76S080764Spar · corrodedDURING SHOP VISIT, CORROSION WAS FOUND ON THE REAR SPAR OF THE RT INBOARD MAIN FLAP. THE DAMAGE WAS CUT OUT AND A REPLACEMENT SECTION WAS SPLICED IN. REPAIR WAS COMPLETED PER ERA 467064-14.May 20, 2008 · N121DE · Boeing 767332SDR SWAA082752Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM.May 20, 2008 · N705SW · Boeing 7377H4SDR 08FDEA01887Skin · dentedRT WING INBD FLAP LOWER SURFACE FOUND WITH 2 DENT MARKS.May 20, 2008 · N590FE · Doug MD11F
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