JASC 5753

Service difficulty reports · 31,496

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 FDEA202504170604Skin · no discrepancyEXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB10-RIB12 BETWEEN S2.2 AND REAR SPAR REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB10-RIB12 BETWEEN S2.2 AND REAR SPAR WAS EVALUATED AND FOUND NOT IN CONFORMITY Apr 17, 2025 · N676FE · Airbus A300F4605RSDR SWI2025F00930Attach Angle · corrodedTHE LT MLG TIRE BURST PANEL 542AZ ATTACHMENT ANGLE IS CORRODED. INSTALLED NEW LT MLG TIRE BURST PANEL 542AZ ATTACHMENT ANGLE REF. DWG CC670-10320, REV -F AND SRM 51-42-21-001-001-A01. COMPLETED SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.Apr 16, 2025 · N802SK · Cndair CL6002D24SDR SWIA2025071600416Vane · damagedNOTCH NOTED AT R/H INBD FLAP VANE ACUTATOR COMMON TO PANEL 684BB (MARKED) (C-CHECK RO 07/15/2025)REMOVED DAMAGE FROM RH INBD FLAP VANE ACTUATOR COMMON TO PANEL 684BB IAW REO 670-57-52-257 REV -A, DATED: 2024-08-20. OPS CHECK GOOD AT THIS TIME. COMPLIED WITH Apr 16, 2025 · N802SK · Cndair CL6002D24SDR SWAA2025042325560Panel · wornLEFT WING AFT UPPER TRAILING EDGE PANEL ATTACH POINT ON THE INBOARD UPPER PANEL ATTACH BEAM WAS WEAR (BEAM ON THE INBOARD SIDE OF DEFLECTION RIB). <[01] LEFT WING AFT UPPER TRAILING EDGE SUPPORT BEAN PANEL SEAL REQUIRE TO BE REMOVE TO FOM; [02] REMOVED SUPPORTApr 16, 2025 · N421LV · Boeing 7377H4SDR FDEA202504150593Skin · unknownDURING AGING INSP. FOUND EXISTING REPAIR ON O/B LOWER FLAP 102" TO THE O/B EDGE, LH O/B AFT FLAP. COMPLIED WITH - EA # F - 5750-T0383010 P1 TITLE: WINGS - FLIGHT SURFACES - LH WING OTBD. AFT FLAP LOWER SKIN REPAIR, RSC TRACKING. THIS IS MAJOR REPAIRApr 15, 2025 · N985FD · Boeing 757230SDR FDEA202504150592Skin · unknownDURING AGING INSP. FOUND EXISTING REPAIR ON O/B LOWER FLAP 14.5" TO THE I/B EDGE, LH O/B AFT FLAP. COMPLIED WITH EA # F-5750-T0383010 P1. THIS IS MAJOR REPAIR.Apr 15, 2025 · N985FD · Boeing 757230SDR WRXR20250415001Hinge Fitting · gougedON RIGHT OUTBOARD FLAP, MIDDLE HINGE LUG LOWER FITTING, SMALL DENT WAS DISCOVERED. DEPTH OF GOUGE READS AT .0085". BLENDED DAMAGE IAW CRJ 900 SRM 51-71-00-001-001-A01. ROTO-PEENED REWORKED AREA IAW CRJ 900 SRM TASK 51-24-11-001-001-A01 AND REO 690-57-53-165.Apr 15, 2025 · N638NN · Cndair CL6002D24SDR CALA2025042204111Doubler · corrodedLH WING O/B FLAP RIB 5-6, TRACK 3 SUPPORT, INTERNAL DOUBLER FOUND CORROSION AROUND SEVERAL FASTENERS.Apr 14, 2025 · N459UA · Airbus A320232SDR CALA2025042204110Doubler · corrodedRH WING O/B FLAP RIB 5-6, TRACK 3 SUPPORT, INTERNAL DOUBLER FOUN D CORROSION AROUND FASTENERS. INSTALLED FLAP.Apr 14, 2025 · N459UA · Airbus A320232SDR SWAA2025041524243Skin · debondedLEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE<[01] REMOVED LH OTBD TRAILING EDGE FLAP PER M/M 27-51-22;[02] INSTALLED LH OB TRAILING EDGE FLAP REF MM 27-51-22Apr 13, 2025 · N417WN · Boeing 7377H4SDR FDEA202504120653Skin · corrodedAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN AT RIB27,T/E-2" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR Apr 12, 2025 · N677FE · Airbus A300F4605RSDR FDEA202504120643Skin · dentedAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON LH O/B FLAP L/E NOSE BTW RIB14~RIB18 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 1Apr 12, 2025 · N677FE · Airbus A300F4605RSDR IPXA2025052368348Rib · cracked**SUPPLEMENTAL SDR** FAULT: L/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-93428-REQ1 AND VT-MAE EA 300-5750-27-A3891, REV. -. REVIEWEDApr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025052368187Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (2) CRACK INDICATION AND HAS BEEN MARKED IN RED. INSTALLED NEW ANGLE FOR R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27 FLANGER REPAIR BETWEEN STRINGER 2.6 AND STRINGER 2.7 AND 2.8 AND REAR SPART IAW A30Apr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025052368253Rib · crackedL/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. ACCOMPLISHED WHIT E.A 300-5750-27-A3891 PRELIMINRY 1 AND INSTALLED DOUBLER AT CENTER FLAP LH IN ACCORDANCE WHIT SRM 57-50-00 AND MATERIAL USED 2024T3 0.05Apr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025052368088Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93431-REQ1 AND VT-MAE EA 300-5750-27-A3892, REV. -. REVIEWEDApr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025042668348Rib · crackedL/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3891 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025042668088Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025042668253Rib · crackedL/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3891 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025042668187Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (2) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622RSDR IPXA2025042668077Rib · crackedSDR FILED OPEN. R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27F HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1.Apr 11, 2025 · N125UP · Airbus A300F4622RSDR 21GA202504160002Fitting · damagedRH FAIRING SUPPORT #7 FLAP REPAIR.Apr 11, 2025 · N765CK · Boeing 7673P6SDR 21GA202504161010Fitting · crackedRH FAIRING IB #7 FLAP SUPPORT CRACK REPAIR.Apr 11, 2025 · N765CK · Boeing 7673P6SDR 21GA20250411007Support Fitting · damaged#1 FLAP SUPPORT FITTING FASTNER HOLE DAMAGED.Apr 11, 2025 · N765CK · Boeing 7673P6SDR 21GA20250411005Support Fitting · damagedLH FAIRING SUPPORT #1 FLAP FITTING ASSY DAMAGED.Apr 11, 2025 · N765CK · Boeing 7673P6SDR SWIA2025082500410Skin · damagedRIGHT INBD FLAP LOWER SKIN BETWEEN FLS65.50-FLS75.60 AT TRAILING EDGE LIGHTNING STRIKE DAMAGE. PER REO 690-57-52-517 DATED 2025-04-07 REV TEMPORARY DISPOSITION FOR BLENDED LIGHTNING STRIKE DAMAGE ON RH INBD FLAP LOWER SKIN BETWEEN FLS65.50-FLS75.60 AT TRAILINGApr 10, 2025 · N804SK · Cndair CL6002D24SDR G1IA20250410089Flap Track · crackedON PREFLIGHT, THE PILOT NOTICED THE RH OUTBOARD FLAP SEEMED LOSE. WE HAD A MECHANIC INSPECT THE OUT OF SERVICE EVENT AND FOUND THE OUTBOARD FLAP TRACK CRACKED.Apr 10, 2025 · N400EM · Beech C90ASDR DALA2025042303178Strut · corrodedSHIP 3084 CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: THE INTERCONNECTING STRUT PN: D5757030501600 & SN:A24158 WAS REMOVED IN UNSERVICEABLE CONDITION BY MISTAKE BY MAINTENANCE , UPDATED THE PART WAS REMOVED ON SERVICEABLE CONDITION. Apr 10, 2025 · N384DN · Airbus A321211SDR SWAA2025041423226Skin · debondedLEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN HAS MISSING AND DISBONDED/DEFORMED MATERIAL ON THE INBD EDGE AND 10IN FROM THE TRAILING EDGE.<[01] PERFORMED EA- 25-157-00935;[02] VERIFIED THAT MAINTENANCE ACTIONS HAVE BEEN COMPLIED WITH IAW EA 25-157-00935;[03] VEApr 10, 2025 · N417WN · Boeing 7377H4SDR G1IA202504140089Flap Track · crackedON PREFLIGHT THE PILOT NOTICED THE RH OUTBOARD FLAP SEEMED LOOSE. WE HAD A MECHANIC INSPECT THE OUT OF SERVICE EVENT AND FOUND THE OUTBOARD FLAP TRACK CRACKEDApr 10, 2025 · N400EM · Beech C90ASDR DALA2025102407791Hinge Fitting · corrodedLT FLAP I/B FWD HINGE FITTING MOUNT PINS ON REAR SPAR CORRODED 4EA. REPAIRED PER ERA 620694-14AD. (0904194)Apr 9, 2025 · N925AT · Boeing 717200SDR SWI2025F00774Beam · damagedLH INBOARD FLAP FLS 140.40 VANE ACTUATOR BEAM HAS ROLLER INDENTIONS (C-CHECK RO 06/29/2025)LH INBOARD FLAP FLS 140.40 VANE ACTUATOR BEAM PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. OPERATIONAL TEST PASSED. COMPLIED WITH M-337 ANDApr 9, 2025 · N800SK · Cndair CL6002D24SDR SWIA2025070100409Roller · damagedLH INBOARD FLAP FLS 24.0 VANE ACTUATOR BEAM HAS ROLLER INDENTIONS (C-CHECK RO 06/29/2025)LH INBOARD FLAP FLS 24.0 VANE ACTUATOR BEAM REPAIRED PER REO 670-57-52-257 REV -A DATED 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 AND TASK CARD 51-900-10Apr 9, 2025 · N800SK · Cndair CL6002D24SDR NACA2025040800008Skin · debondedRH WING OUTBOARD AFT FLAP LOWER SKIN DISBOND BETWEEN WBL.270~WBL.280. PERFORMED CATEGORY A METAL BOND REPAIR WITH 250 F CURE MATERIAL AT RH WING OUTBOARD AFT FLAP LOWER SKIN BETWEEN WBL 270-WBL 280 IAW B737-300 SRM 57-53-02 REPAIR 2 & SRM 51-70-10 REPAIR 4 (R1Apr 8, 2025 · N360WA · Boeing 737301SDR SWI2025F00785Rod · damagedRH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 102.90. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR ROD AT APPROX FLS 102.90. REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. OPERATIONAL TEST PASSED. COMPLIED WITHApr 8, 2025 · N800SK · Cndair CL6002D24SDR SWI2025F00783Rod · groovedRH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 140.40. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR AT APPROX FLS 140.40 REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 AND TASK CAApr 8, 2025 · N800SK · Cndair CL6002D24SDR SWI2025F00782Rod · damagedRH INBD FLAP VANE ACTUATOR AT APPROX FLS 24.00 HAS A GROOVE ON THE ACTUATOR ROD. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR AT APPROX FLS 24.00 REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 ANApr 8, 2025 · N800SK · Cndair CL6002D24SDR SWI2025F00780Rod · groovedRH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 65.50. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR ROD AT APPROX FLS 65.50 REPAIRED PER REO 670-57-52-257 REV-A DATE 2024-08-20. WITHIN LIMITS. OPERATIONAL TEST PASSED. COMPLIED WITH M-337 Apr 8, 2025 · N800SK · Cndair CL6002D24SDR SWIA2025070100408Track · damagedRH INBD FLAP HAS GROOVES ON THE VANE ACTUATOR CAM TRACKS AT APPROX FLS 102.90. REPAIRED RH INBD FLAP ON THE VANE ACTUATOR CAM TRACKS AT APPROX FLS 102.90 BY COMPLYING WITH ALL STEPS OF REO 670-57-52-259 REV -.Apr 8, 2025 · N800SK · Cndair CL6002D24SDR IXX2025F00008Skin · delaminatedL/H O/B T/E DELAMINATION OF FLAPApr 8, 2025 · N431AZ · Boeing 767381SDR IXXA20250408001Skin · delaminatedL/H I/B T/E DELAMINATION OF FLAP.Apr 8, 2025 · N431AZ · Boeing 767381SDR JR2R20250408280Doubler · crackedRIGHT HAND OUTBOARD FLAP TRACK 4 COMPOSITE DOUBLER IS CRACKED AND DELAMINATED.Apr 8, 2025 · N88326 · Emb ERJ170200LRSDR FDEA202504080581Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 3 IN AWAY TO AFT EDGE AND 213 IN TO IB EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 247 AS PER B777 SRM 57-53-01-2R- 2 AND SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-T0382953 P1. THIS IS A MAJOR REPAIRApr 8, 2025 · N849FD · Boeing 777FSDR SWAA2025040922278Flap · delaminatedRH OUTBOARD AFT FLAP (PN: 113A3700-20; SN: 997) UPPER SKIN DELAMINATION AT INBOARD EDGE <[01]. REMOVED R/H O/B AFT. FLAP PER AMM 27-51-22; [02] OK TO INSTALL NEW FLAP; [03] INSTALLED RH OB AFT FLAP PER AMM 27-51-22.; [04] INSTALLED RH OB AFT FLAP PER AMM 27-5Apr 7, 2025 · N444WN · Boeing 7377H4SDR NACA2025040500004Skin · gougedGOUGE WAS FOUND AT LH WIN O/B FORE FLAP NOSE LOWER SKIN , WBL 412.11. MADE REPAIR PARTS. INSTALL REPAIR PARTS AT LH WIN O/B FORE FLAP NOSE LOWER SKIN PER: 737-300 SRM 57-53-01 REPAIR 1. (R136)"Apr 5, 2025 · N360WA · Boeing 737301SDR SWAA2025050722023Skin · debondedDEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE PANEL AT LT WING. PERFORMED PERMANENT REPAIR ON I/B MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SKIN AT LT WING IAW EA# 25-157-01004.Apr 5, 2025 · N941WN · Boeing 7377H4SDR SWAA2025050622022Skin · debondedDEBONDED EXTERNAL SKIN OB AFT FLAP IB EDGE AT RT WING. 2025-243970<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.;[02] TOOL USED STEP 3: ULTRASONIC EQUIPMENT; P/N: BONDMASTER 600M; S/N: 230106912; DUE DATE: 05 FEB 2026.;[03] TOOL USApr 5, 2025 · N941WN · Boeing 7377H4SDR SWAA2025040821719Skin · debondedRIGHT OUTBOARD AFT FLAP UPPER SKIN DISBONDED AT INBOARD EDGE; 10 INCHES FROM AFT EDGE (NOT DELAMINATED)<[01] REPAIRED PER EA 25-157-00897.Apr 5, 2025 · N444WN · Boeing 7377H4SDR DALA2025040702671Roller · excess playSHIP 3313 RHW O/B FLAP UPLOCK ROLLER TOO MUCH PLAY. CORRECTIVE ACTION: R/R ROLLERS PER A330 AMM 27-54-73. OK FOR SERVICE. (0896729)Apr 5, 2025 · N813NW · Airbus A330323SDR NACA2025040400001Skin · chafedRH WING INBOARD FORE FLAP SKIN WORN AT WBL.73. REMOVED THE DAMAGED DOUBLER AT RH WING INBOARD FORE FLAP SKIN AT WBL.73. PERFORMED CATEGORY A METAL BONDING WITH250 F CURE MATERIAL. IAW B737-300 SRM 57-53-02 REPAIR 1 & SRM 51-70-10 REPAIR 4 (REV136).Apr 4, 2025 · N360WA · Boeing 737301
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