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 SWAA082008Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 FLAP TRACK AFT SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.Apr 14, 2008 · N359SW · Boeing 7373H4SDR SWAA082007Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 1 FLAP TRACK AFT SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.Apr 14, 2008 · N359SW · Boeing 7373H4SDR SWAA081990Skin · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Apr 14, 2008 · N345SA · Boeing 7373K2SDR UIEA200800155Access Panel · corrodedRIGHT WING TRAILING EDGE INBOARD MIDFLAP LOWER SURFACE ACCESS PANEL WBL 240.00 HAS SIGNS OF CORROSION. REMOVED AND REPAIRED CORROSION AT WBL 240.00 PER SRM 57-40-20.Apr 13, 2008 · N526MC · Boeing 7472D7BSDR SWAA081978Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 8 FLAP TRACK OUTBOARD FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.Apr 13, 2008 · N510SW · Boeing 7375H4SDR SWAA081945Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD MIDFLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.Apr 13, 2008 · N354SW · Boeing 7373H4SDR USAA920080917Flap · delaminatedMCN - MAJOR REPAIR - C21 CHECK - LEFT WING OUTBOARD FOREFLAP HAS DELAMINATED AREA, WBL 278.69 - WBL 280.69. REPAIRED LEFT WING OUTBOARD FOREFLAP, WBL 278.69 - WBL 280.69 IAW B737 SRM 51-70-10-2R4.Apr 12, 2008 · N164AW · Boeing 73733ASDR 2008UALA02085Structure · damagedLT INBD FLAP TRAILING EDGE HAS DAMAGE. REPLACED FLAP ASSEMBLY.Apr 11, 2008 · N306UA · Boeing 737322SDR MALA080056Rib · crackedRT FLAP, AFT COVE FAIRING RIB IS CRACKED. REPLACED RT FLAP AFT COVE FAIRING RIB P/N 7257840-082 IAW SRM 51-40-23. REMOVED AND REPLACED TURTLE BACK FAIRING TO FACILITATE REPAIR IAW SRM 51-40-23. RT FLAP ASSEMBLY REMOVED AND INSTALLED TO FACILITATE REPAIR PERApr 10, 2008 · N445XJ · Saab 340BSDR A6WA200840312Skin · dentedDENT ON RT OUTBOARD WING FLAP. RT OUTBOARD WING FLAP REPAIRED IAW SRM 57-53-00 FIG 202 SHEET 2 REPAIR 3. (A)Apr 9, 2008 · N403AW · Cndair CL6002B19SDR 2008UALA02068Skin · damagedLT WING INBD FLAP UPPER MID SURFACE OTBD DEPTH WEAR LINE IN PREVIOUS REPAIR. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW METAL DOUBLER.Apr 9, 2008 · N535UA · Boeing 757222SDR UPS08852180Link · gougedINSPECTION TYPE:C1 LEFT WING I/B ATTACH LINK AT STA XW 106 HAS DEEP GOUGE. BLENDED GOUGE, REWORKED FINISH AND HFEC, FLAP PEENED IAW SRM EO 008-2 760-01-A1360, DPS 4.999-2, 57-2-0.Apr 8, 2008 · N803UP · Doug DC873FSDR A6WA200840303Angle · brokenLEFT WING OUTBOARD FLAP, INBOARD HINGE ARM, LEFT ANGLE IS BROKEN. (M) ANGLE FABRICATED IN S6144-13 IAW SRM 51-24-36 PRIMER AND PAINT APPLIED IAW SRM 51-25-01 AND INSTALLED IAW SRM 51-42-06. (A)Apr 8, 2008 · N403AW · Cndair CL6002B19SDR A6WA200840292Bracket · brokenBRACKET BROKEN AT THE CENTER HINGE ARM OF THE RIGHT WING OUTBOARD FLAP. (M) BROKEN BRACKET AT CENTER HINGE ARM OF RIGHT WING OUTBOARD FLAP REPLACED IAW SRM 51-42-06.Apr 7, 2008 · N403AW · Cndair CL6002B19SDR 2008UALA02004Skin · damagedFOUND RIGHT OTBD FLAP HAS A HOLE AND A DENT AT THE MIDDLE AFT SECTION. REPAIRED DAMAGED AREA OF FLAP. (POTTED COMPOSITE REPAIR)Apr 7, 2008 · N829UA · Airbus A319131SDR WRLA2008042Hinge Fitting · crackedLEFT OUTBOARD FLAP CENTER BOX INBOARD AFT HINGE SUPPORT CRACKED. R&R LT OUTBOARD FLAP IAW AMM 27-60-30.Apr 7, 2008 · N380WA · Doug MD11FSDR DHL2008760512Skin · dentedEVALUATED DENT/EXCEEDS LIMITS, FABRICATED AND INSTALLED FLUSH REPAIR ON RT I/B MID FLAP UPPER SKIN AT RWBL 110 PER B727 SRM 57-50-2 FIG 3 AND 57-50-4 FIG 2.Apr 6, 2008 · N760AT · Boeing 7272B7SDR VNAA0804005Flap · damagedCREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT HAND INBOARD FLAP TRAILING EDGE AND REPAIRED THE DAMAGE UNDER REO 601R-57-52-732 AND THE AIRCRAFT MAIApr 5, 2008 · N216PS · Cndair CL6002B19SDR CPCP20080024Retainer · corrodedRT OUTB FLAP RIB 19 BRUSH RETAINER IS CORRODED. RT OUTB FLAP RIB 19 BRUSH RETAINER REPLACED IAW SRM 51-25-03.Apr 4, 2008 · N348AE · Aerosp ATR72212SDR DLM88080559Skin · dentedDURING HMV A DENT WAS FOUND ON LOWER SKIN OF OUTBD GUIDE VANE LT OUTBD FLAP. VANE WAS REPAIRED IAW SRM 51-70-2D.Apr 4, 2008 · N962DL · Doug MD88SDR 2008UALA01929Panel · wornWEAR WAS FOUND ON THE PANEL OF THE RT WING T/E OUTBOARD FLAP UPPER SURFACE, O/B END L=35". DID NDT INSP PER NDT MANUAL PART1. 51-01-01 FIG 9, NO DELAMINATION. REPAIRED REF 777EN-57-0031-01, TOUCH-UP PAINT REF AMM 51-21-10P701.AC OK FOR SERVICE.Apr 4, 2008 · N798UA · Boeing 777222SDR 2008UALA01928Panel · wornWEAR WAS FOUND ON THE PANEL OF THE RT WING T/E OUTBOARD FLAP UPPER SURFACE NEAR MID POINT L=50". DID NDT INSP PER NDT MANUAL PART1. 51-01-01 FIG 9, NO DELAMINATION. REPAIRED REF 777EN-57-0031-01, TOUCH-UP PAINT REF AMM 51-21-10P701.AC OK FOR SERVICE.Apr 4, 2008 · N798UA · Boeing 777222SDR 2008UALA01927Panel · wornWEAR WAS FOUND ON THE PANEL OF THE RT WING T/E OUTBOARD FLAP UPPER SURFACE, INBOARD END L=31". DID NDT INSP PER 777 NDT MANUAL PART 1. 51-01-01 FIG 9, NO DELAMINATION, REPAIRED PER 777EN-57-0031-01, TOUCH UP PAINT REF TO AMM 51-21-10 P701.AC OK FOR SERVICE.Apr 4, 2008 · N798UA · Boeing 777222SDR 2008UALA01926Plate · wornHONEYCOMB PLATE WEAR WAS FOUND AT UPPER SURFACE OF LEFT WING OUTBOARD FLAP. DID NDT INSP PER NDT MANUAL PART1 51-01-01 FIG 9, NO DELAMINATION. REPAIRED REF 777EN-57-0030-01, TOUCH UP PAINT PER AMM 51-21-10P701. AC OK FOR SERVICE.Apr 4, 2008 · N798UA · Boeing 777222SDR 08FDEA01290Skin · delaminatedLT I/B FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE, WS 275 CUT OUT DELAMINATED AREA 7 1/2 INCH BY 7 1/2 INCH ON LT I/B FORG FLAP UPPER SURFACE AND REMOVED DAMAGED CORE 7 1/2 BY 7 1/2. SHAPED SECTION OF CORE 7 1/2 INCH BY 7 1/2 INCH. FABRICATED DOUBLERApr 3, 2008 · N466FE · Boeing 727225SDR 08FDEA01303Skin · damagedLT FLAP VANE L/E SKIN CHAFED AT NR 3 TRACK ATTACH POINT. GENERATED RFTS N425FE-25-33028. RECEIVED EA NR 6-5750-118464. REMOVED FASTENER FROM BLENDED AREA. HFEC INSPECTED THE HOLE PER NTM 51-10-01 PART 6. NO FINDINGS. INSPECTED BLENDED AREA PER NTM 51-10-Apr 2, 2008 · N425FE · Airbus A310203SDR WRLA2008040Hinge Fitting · crackedDURING C-CHECK INSPECTION FOUND LEFT OUTBOARD FLAP CENTER BOX INBOARD AFT HINGE SUPPORT FITTING CRACKED. REMOVED AND REPLACED HINGE WITH NEW PARTS IAW MD11 SRM VOL.II 51-33-01 REV.40Apr 2, 2008 · N380WA · Doug MD11FSDR 08FDEA01255Skin · dentedLEFT WING, INBOARD FLAP LOWER SKIN FOUND WITH DENT AT STA XIFH 299. DENT AREA MEASURED AND FOUND OUT OF LIMIT PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Apr 2, 2008 · N584FE · Doug MD11FSDR 08FDEA01253Skin · dentedRIGHT WING, INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 150. DENTED AREA MEASURED FOUND OUT OF LIMIT PER SRM 57-10-00 FIGURE 17 VOLUME I. DEPTH = 0.048" AND DIAMETER = 0.5". REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOApr 2, 2008 · N584FE · Doug MD11FSDR 08FDEA01416Panel · delaminatedRIGHT WING INBD FLAP PANEL 644 AB IS DISBONDED. REPAIRED PANEL 644 AB BY REMOVING DAMAGED OUTER SKIN; INNER AND OUTER DOUBLERS. FABRICATED AND BONDED NEW SKIN; INNER AND OUTER DOUBLERS IAW DAC DWG NR ARC 2991; TPS 101, REV E AND FEDEX EA 8-5750-118470 TITLEApr 1, 2008 · N365FE · Doug MD1010FSDR 08FDEA01236Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE AT STA XIFH 162 TO XIFH 175 FROM THE FRONT SPAR PLANE TO THE REAR SPAR PLANE HAS 3 EA DENTS THAT REQUIRE REPAIR. CUT OUT DAMAGE IN REF TO SRM 57-10-00 FIG 85 VOL I. FABRICATED DOUBLERS IN REF TO SRM 57-10-00 FIG 85 VOL I. Apr 1, 2008 · N365FE · Doug MD1010FSDR 08FDEA01220Paint · missingPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP LOWER MAIN SKIN BETWEEN RIBS 3 AND 4 MEASURES 10.4" BY 9.9". REPAIR NOT IAW SRM REQUIREMENTS DUE TO REPAIR DOUBLER MISSING FILLET SEAL AND PAINT. REPAIRED PROTECTIVE COATING AND RESEALED EDGApr 1, 2008 · N448FE · Airbus A310222SDR 08FDEA01219Seal · missingPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP LOWER MAIN SKIN BETWEEN RIBS 4 AND 5 MEASURES 10.6 INCHES BY 9 INCHES. REPAIR NOT IAW SRM REQUIREMENTS DUE TO REPAIR MISSING FILLET SEAL AND PAINT. REPAIRED PROTECTIVE COATING AND RE-SEALED Apr 1, 2008 · N448FE · Airbus A310222SDR USAA920080877Structure · crackedBFM - MAJOR REPAIR - LEFT WING INBOARD FLAP TRAILING EDGE CRACKED. REPAIRED LEFT WING INBOARD FLAP TRAILING EDGE CRACKED IAW B757 SRM 57-53-01.Mar 31, 2008 · N921UW · Boeing 757225SDR USAA920080836Skin · delaminatedCLT - MAJOR REPAIR - C22 CHECK - A 2.25" X 1.75" AREA OF DELAMINATION ON RIGHT O/B TRAILING EDGE FOREFLAP ON TOP SURFACE. INSTALLED REPAIR IAW SRM 51-70-10 REPAIR 3 AND 4.Mar 31, 2008 · N175AW · Boeing 73733ASDR MASA200800282Flap Track · wornRIGHT NR 5 FLAP TRACK WORN UPPER, LOWER, AND MID. REPAIRED FLAP TRACK.Mar 31, 2008 · N988HA · Dhav DHC8202SDR MASA200800281Flap Track · wornLEFT NR 4 FLAP TRACK WORN UPPER, LOWER, AND MID. REPAIRED FLAP TRACK.Mar 31, 2008 · N988HA · Dhav DHC8202SDR MASA200800280Flap Track · wornRIGHT NR 4 FLAP TRACK WORN UPPER, LOWER, AND MID. REPAIRED FLAP TRACK.Mar 31, 2008 · N988HA · Dhav DHC8202SDR MASA200800279Flap Track · wornLEFT NR 5 FLAP TRACK WORN UPPER, LOWER AND MID. REPAIRED FLAP TRACK.Mar 31, 2008 · N988HA · Dhav DHC8202SDR 08FDEA01214Skin · dentedRIGHT OUTBD FLAP LOWER SURFACE AT STA XOFH 703 HAS A DENT. CHECKED DENT, NOTED CREASES. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00; FIG 48; VOL I. MATERIAL ID FOR THE REPAIR DOUBLER IS 2024-T3, 0.050, PO 610199.1. FABRICATED DOUBLER IAW DC/MD-10 SMar 31, 2008 · N365FE · Doug MD1010FSDR 08FDEA01213Skin Panel · dentedLEFT INBD FLAP LOWER SURFACE FWD PANEL 2ND FROM THE OUTBD END HAS 1 DENT. REMOVED LEFT FLAP LOWER SURFACE PANEL TO FOM IN REF TO DC/MD-10 SRM 51-31-01; VOL II. REPAIRED GOUGED DENT IN REF TO DC/MD-10 57-00-01; FIG 1 A; SHEET 2. INSTALLED PANEL IN REF TO DC/Mar 31, 2008 · N365FE · Doug MD1010FSDR QXEA200800348Flap Track · wornPDX-C5 CHECK- LT NR 3 FLAP TRACK HAS SEVERAL AREAS OF WEAR ON THE LOWER HORIZONTAL TRACK UPPER SURFACE APPROX .500 INCHES BY .300 INCHES BY .010 DEEP. BLENDED AFFECTED AREAS ON NR 3 FLAP TRACK LOWER HORIZONTAL UPPER IAW RD8-57-987. HFEC INSPECTED BLENDED AREMar 30, 2008 · N356PH · Dhav DHC8202SDR QXEA200800367Flap Track · wornPDX-C4 CHECK - LT WING NR 5 FLAP TRACK OUTBOARD LOWER TRACK UPPER SURFACE HAS WEAR MARKS. BLENDED IAW RD8-57-989. HFEC INSPECTED IAW D8-200 NDTM PART 651-00-01. NO CRACKS NOTED. (S)Mar 30, 2008 · N356PH · Dhav DHC8202SDR ASAA0842855Skin · dentedLT OUTBOARD T/E AFT FLAP LWR SKIN HAS 3 DENTS AT WBL 231.5 TO 240 2.5" FROM T/E. REPAIRED WITH REPAIR PART.Mar 30, 2008 · N796AS · Boeing 737490SDR SWAA081713Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.Mar 30, 2008 · N676SW · Boeing 7373A4SDR ASAA0842857Skin · gougedRT OUTBOARD T/E FORE FLAP L/E GOUGED, REPAIRED WITH REPAIR PART.Mar 29, 2008 · N796AS · Boeing 737490SDR 08FDEA01200Skin · dentedRIGHT INBD FLAP LOWER SURFACE FWD PANEL; 2ND FROM THE INBD END HAS SEVERAL DENTS. REMOVED PANEL IAW DC/MD-10 SRM 51-31-01; VOL II. DEPTH OF THE DENTS ARE 0.125 THRU 0.325 USING DEPTH GAUGE T8492C. ORIGINAL THICKNESS OF THE SKIN IS 0.040 IAW DC/MD-10 SRM 57-Mar 28, 2008 · N365FE · Doug MD1010FSDR SWIA200819401Flap · damagedFLT 3773 - OUTBOARD, RIGHT FLAP WAS DAMAGED BY BIRD STRIKE. REPLACED RIGHT, OUTBOARD FLAP IAW MM 27-54-05. OPS CHECK GOOD. Mar 28, 2008 · N454SW · Cndair CL6002B19SDR 08FDEA01196Skin · dentedRIGHT INBD FLAP LOWER SURFACE AT STE XIFH 255 HAS A DENT. DEPTH OF THE DENT IS .225. ORIGINAL THICKNESS OF THE SKIN IS 0.040. OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; FIG 1A; VOL I. USED DEPTH GAUGE TWS 8358A IAW DC/MD-10 SRM 57-00-01; FIG 1 A; VOL I. REMMar 28, 2008 · N365FE · Doug MD1010FSDR CALA0800273Carriage · corrodedNR 3 MID FLAP CARRIAGE, BOTH ARMS PITTED WITH CORROSION. REMOVED AND REPLACED WITH SERVICEABLE I/B AND O/B CARRIAGE HALVES ON O/B SIDE OF NR 3 MID FLAP.Mar 28, 2008 · N46625 · Boeing 737524
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