JASC 5753

Service difficulty reports · 31,493

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 AALA202512034946Wedge · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING INBOARD FLAP OUTBOARD WEDGE ON MAIN FLAP DELAMINATED INSTALLED REPAIRED FLAP WEDGE. PER SRM 51-40-02.Nov 12, 2025 · N946NN · Boeing 737823SDR CALA2025111411214Skin · debondedRIGHT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN DEBONDED AREAS NOTED, AREA NR 1 L=1.25 INCH W=1 INCH, AREA NR 2 L=1 INCH W=1 INCH.. CLEANED, PREPPED, PERFORMED THE PERMANENT REPAIR AND RESTORED FINISHED ON RT WING OTBD AFT FLAP UPPER SKIN IAW SRM 57-53Nov 11, 2025 · N16713 · Boeing 737724SDR GTIA2025111339175Skin Panel · corrodedPERFORATION ON LEADING EDGE. SKIN OB FLAP OB SIDE ON RT WING RAF-01 3524656-02 GENERATED. PERFORMED PERMANENT REPAIR LOC. ON LEADING EDGE SKIN OB FLAP OTBD SIDE ON RT WING IAW SRM 57-53-00-300-029.Nov 11, 2025 · N696NK · Airbus A320232SDR AALA202512038211Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT ATTACH FITTING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-72-11.Nov 10, 2025 · N831AW · Airbus A319132SDR SWAA2025120233464Support Beam · crackedCRACK TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM AT LT WING. PERFORMED PERMANENT REPAIR ON TRAILING EDGE DEFLECTION CONTROL RIB UPPER SUPPORT BEAM AT LT WING IAW SRM 57-51-02-2R-3, REPAIR 3.Nov 9, 2025 · N462WN · Boeing 7377H4SDR DALA2025111008194Flap Track · corrodedCORROSION ON OTBD FLAP BEARING HOUSING AT TRACK 3 LT WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 629676-14. (1295851).Nov 9, 2025 · N353NB · Airbus A319114SDR SWAA2025112033159Bracket · crackedL/H WING: PANEL 551FB DUAL NUT PLATE BRACKET IS CRACKED. BRACKET IS ON THE FWD EDGE OF PANEL; JUST INBD OF THE GREEN TEE ANGLE. REMOVED AND REPLACED PANEL 551FB DUAL NUT PLATE BRACKET IAW SRM 51-40-02.Nov 8, 2025 · N8507C · Boeing 7378H4SDR FDEA202511082151Flap · damagedPUNCTURE ON LOWER SKIN OF AFT INBOARD TRAILING EDGE FLAP RH WING, APPROX 6.250" OF INBOARD EDGE AND 0.500" OF LOWER EDGE. PUNCTURE ON LOWER SKIN OF AFT INBOARD TRAILING EDGE FLAP RH WING WAS EVALUATED AND WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 DETANov 8, 2025 · N158FE · Boeing 7673S2FSDR Y9PA2025111010000Flap · not reportedRIGHT HAND ON THIS AIRCRAFT WHILE THE ORIGINAL FLAP WAS REMOVED FOR REPAIR. NEEDED TO GROUND THE ACFT TO VERIFY THE FLAP. THEY STATED THE FLAP WAS NOT PROPERLY IDENTIFIED WHEN INSTALLED. THEY PROCEDDED TO SEND A MECHANIC TO THE AIRCRAFT TO VERIFY STATUS OF THENov 7, 2025 · N650FJ · Gulstm GVISDR DALA2025110708129Roller · wornRT WING OUTBD FLAP - OUTBD GUIDE ROLLER IS WORN. REPLACED WORN ROLLER PER A330 AMM 27-54-73. (1292527)Nov 7, 2025 · N426DZ · Airbus A330941SDR SWAA2025112032160Angle · crackedLEFT WING UPPER TRAILING EDGE ANGLE CRACKED INBD OF MID SPAN DEFLECTION RIB. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-B00069. INSPECTION COMPLETED ON CORRECTIVE ACTION NR 1 FOR REPLACEMENT OF ANGLE.Nov 6, 2025 · N8510E · Boeing 7378H4SDR SWAA2025110732216Skin · delaminatedLEFT WING OTBD AFT FLAP, INBD LOWER CORNER DELAMINATED ON TOP SKIN WHICH MEASURES 13 X 8 AND BOTTOM SKIN WHICH MEASURES 9 X 5. BOTH SURFACE SKIN EDGES ARE NOT DELAMINATED IAW EA 25-127-03054.Nov 6, 2025 · N7750A · Boeing 7377BDSDR DALA2025110708118Clamp · wornSHIP 3163 WEAR ON CLAMP TRUNNION IB FLAP ON LH WING. CORRECTIVE ACTION: R/R CLAMP TRUNNION IB FLAP ON LH WING AS PER AIRBUS CMM 57- 52-21 SUBTASK 57-52-21-350-008-A01. (1291884).Nov 6, 2025 · N363NB · Airbus A319114SDR FDEA202511062138Skin · gougedL/H WING OUTB AFT FLAP UPPER SKIN MIDDLE SECTION WITH GOUGE. GOUGE WITH CRACK AT L/H WING OUTB AFT FLAP UPPER SKIN MIDDLE SECTION WAS REPAIRED IAW B-757 SRM 57-53-01-2R AND SRM 51-70-04-0GNov 6, 2025 · N990FD · Boeing 757232SDR FDEA202511062137Skin · gougedL/H WING OUTB AFT FLAP, UPPER SKIN INB SECTION WITH GOUGE. GOUGE WITH CRACK AT L/H WING OUTB AFT FLAP, UPPER SKIN INB. SECTION WAS REPAIRED IAW B-757 SRM 57-53-01-2R AND SRM 51-70-04-0GNov 6, 2025 · N990FD · Boeing 757232SDR 2025F00259Skin · corrodedRH INBOARD AFT FLAP UPPER TRAILING EDGE SURFACE HAS CORROSION.Nov 6, 2025 · N563NC · Boeing 7673BGSDR 2025F00258Skin · corrodedCORROSION FOUND ON LH I/B AFT FLAP UPPER SURFACE.Nov 6, 2025 · N563NC · Boeing 7673BGSDR FDEA202511062136Skin · gougedRIGHT OTBD FLAP TE AFT FLAP UPPER SURFACE WITH 02 EA GOUGES. GOUGES REPAIRED IAW SRM 57-53-01-2R AND SRM 51-70-17-0G.Nov 6, 2025 · N990FD · Boeing 757232SDR DALA2025110508071Flap Track · corrodedCORROSION ON LT WING OTBD FLAP TRACK NR 3, INNER AND OUTER RIB 5, AT ECCENTRIC BEARING. REPAIRED PER ERA 629676-14. (1287999)Nov 4, 2025 · N353NB · Airbus A319114SDR FDEA202511042123Fairing · dentedRT WING INBD FLAP O/B ACTUATOR AFT FAIRING DENTED. REPAIRED W/H WING I/B FLAP O/B ACTUATOR AFT FAIRING SKIN DENTED DAMGAGE (MPN:113T1770-56G CPN:5721384) IN REF TO B767 SRM 57-53--70-2R FIG. 201 RPR NR 1 SHEET:4.Nov 4, 2025 · N102FE · Boeing 7673S2FSDR DALA2025110408058Strut · corrodedCORROSION ON INTERCONNECTING STRUT OB FLAP ON RH WING. REMOVED INTERCONNECTING STRUT RH WING UNSERVICEABLE CONDITION P/ N D5757032201100 S/N 02507 AS PER A320 FAM AMM 27-51-44-000-001- A STEP 1 THRU 4.A EXCEPT STEP 3.D(2). JOB IN PROGRESS. REPLACED INTERCONNENov 2, 2025 · N361NW · Airbus A320212SDR DALA2025110408057Strut · corrodedSHIP 3261 DISC: CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. C/A: REMOVED INTERCONNECTING STRUT LH WING UNSERVICEABLE CONDITION P/ N D5757032201100 S/N 2285 AS PER A320 FAM AMM 27-51-44-000-001-A STEP 1 THRU 4.A EXCEPT STEP 3.D(2). JOB IN PROGRESS. REPLNov 2, 2025 · N361NW · Airbus A320212SDR SWAA2025111830409Panel · debondedDEBONDED EXTERNAL SKIN UPPER AREA OF WEDGE PANEL LOC ON INBD MAIN FLAP, LT WING. REPAIRED WEDGE PANEL LOC ON INB MAIN FLAP LT WING IAW B737-700 SRM 57-53-01-2R-7 REPAIR 7.Oct 31, 2025 · N455WN · Boeing 7377H4SDR FDEA202510312119Skin · delaminatedDELAMINATION IN LEADING EDGE 8 INCHES FROM THE RIGHT SIDE FACE, OUTBOARD FLAP, LEFT WING LEFT, WING OUTBOARD FLAP LEADING EDGE, 8 INCHES FROM THE RIGHT SIDE FACE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG. 201 SHEET 5 TABLE I AND B767 SRM 51-70-03-Oct 31, 2025 · N156FE · Boeing 7673S2FSDR CALA2025110210814Skin · delaminatedRIGHT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN WITH DISBONDED AREAS 2 X 2.25 INCHES AND 1 X 1 INCHE. REMOVED THE DAMAGED SKIN, CLEANED, PREPPED, FABRICATED NEW REPAIR PARTS, APPLIED PRE-BOND ON NEW REPAIR PARTS, REPAIR AREA AND RESTORED FINISH ON RT WOct 31, 2025 · N16701 · Boeing 737724SDR SWIA2026030275394Skin · chafedRH WING IB FLAP LOWER SURFACE SKIN AT IB FLAP FAIRING LAND HAS SIGNS OF CHAFFING (C-CHECK RO 02/28/2026)REPAIRED DAMAGED SKIN ON RH INBD FLAP LOWER SURFACE IAW BOMBARDIER REO 670-57-52-160 REV-A DATE 2016-10-21 AND CRJ700 550 SERIES SRM 51-26-01, 57-52-01, 5Oct 30, 2025 · N574GJ · Cndair CL6002C11SDR SWIA20260112030Vane · chafedRIGHT INBD FLAP, FLAP VANE LEADING EDGE HAS CHAFE DAMAGE AT (3EA) LOCATIONS. REPAIRED CHAFES ON RH INBOARD FLAP VANE LEADING EDGE INBD AND OTBD LOCATIONS IAW BOMBARDIER REO 601R-57-52-004 THEY WERE WITHIN LIMITS, MID LEADING EDGE WAS OUT OF LIMITS REMOVED ANDOct 30, 2025 · N955SW · Cndair CL6002B19SDR DALA2025110608102Access Panel · delaminatedFOUND RH WING O/B FLAP UPPER ACCESS PANEL 666KT AT 62" FROM I/B SIDE DELAMILATION. RH WING O/B FLAP UPPER ACCESS PANEL 666KT AT 62" FROM I/B SIDE REPAIRED AS PER PRI REV.0 OF ER/A 629898-14. (1277913)Oct 29, 2025 · N837MH · Boeing 767432ERSDR FDEA202510292116Rib · cracked1 EA CRACK (20MM) INDICATION WAS FOUND AT RH WING CENTER FLAP RIB 27 AFTER RIB FLANGE AREA OF TOP SURFACE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB 27, S-2.8 ~ REAR SPAR AND EXTERNAL PLATE REPAIR AT RIB26 ~27, REAR SPAR ~S-2.2. I.A.W FEDEX EA NO:T6-5750-T038Oct 29, 2025 · N690FE · Airbus A300F4605RSDR CALA2025111011086Skin · debondedLEFT WING, OTBD FLAP, AFT FLAP, INBD END, LOWER SKIN WITH TWO DISBONDED AREAS , 4 X 3 INCHES, 6.5 X 3.5 INCHES. CLEANED, PREPPED, PERFORMED A PERMANENT REPAIR AND RESTORED FINISHED IAW SRM 57-53-01-1A-4, SRM 57-53-01-2R-16, SRM 51-70-10-2R- 0, AMM 51-21-41-Oct 28, 2025 · N76288 · Boeing 737824SDR IPXA2025111984916Skin · delaminatedRIGHT WING. OTBD FLAP, CENTER UPPER PANEL HAS DELAMINATION. ACCOMPLISHED REPAIR PER SRM 57-53-01-2R-1 REPAIR 1 FIGURE 201 TABLE III REV 124 AND 250°F CURE IAW SRM 51-70-07-0G-0 PARA 4 REV 124.Oct 27, 2025 · N414UP · Boeing 75724APFSDR IPXA2025103085340Bracket · crackedRIGHT WING CENTER FLAP OUTBD SIDE BRACKET IS BROKEN OFF. INSTALLED BRACKET IAW SRM 51-40-21.Oct 27, 2025 · N126UP · Airbus A300F4622RSDR IPXA2025103085335Bracket · brokenLEFT WING CENTER FLAP OUTBD SIDE BRACKET IS BROKEN OFF. INSTALLED BRACKET IAW A300-600 SRM 51-40-21 P/N CR3223-4-2 BATCH# 0004423484 3EA.Oct 27, 2025 · N126UP · Airbus A300F4622RSDR DALA2025103107968Hinge Fitting · excess playRT WING FLAP O/B HINGE HAS EXCESSIVE PLAY. REPAIRED PER ERA/PRI 629650-14 REV. A (1274899).Oct 27, 2025 · N924AT · Boeing 717200SDR SWAA2025112028732Support Angle · crackedLEFT WING TRAILING EDGE SHELF PANEL AT MAIN FLAP DEFLECTION ROLLER ARM HAS A CRACK IN LATERAL SUPPORT. LOCATED AND DRILLED REPLACEMENT SUPPORT ANGLE IAW SRM 51-40-05.Oct 26, 2025 · N8507C · Boeing 7378H4SDR FDEA202510242087Hinge Bracket · corrodedRIGHT WING :(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORRROSION AT RIGHR HAND WING: (FLAP SIDE) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PEROct 24, 2025 · N603FE · Doug MD11FSDR FDEA202510242086Hinge Bracket · corrodedRIGHT WING :(FLAP SIDE) RIGHT INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING : ( FLAP SIDE ) RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PEOct 24, 2025 · N603FE · Doug MD11FSDR FDEA202510242085Hinge Bracket · corrodedLEFT WING :(FLAP SIDE) LEFT INBOARD FLAP OUTBOARD AFTER HINGE OUTBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING : ( FLAP SIDE ) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MOct 24, 2025 · N603FE · Doug MD11FSDR FDEA202510242084Hinge Bracket · corrodedLEFT WING:(FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFTER HINGE INBOARD PIVOT HOLE AREA FOUND CORROSION. CORROSION AT LEFT HAND WING ( FLAP SIDE) LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE AREA REWORKED AND FOUND EXCEED LIMIT AS PER Oct 24, 2025 · N603FE · Doug MD11FSDR FDEA202510242083Hinge Bracket · corrodedRIGHT WING: WING SIDE RIGHT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORROSION. CORROSION AT RIGHT HAND WING : WING SIDE RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44Oct 24, 2025 · N603FE · Doug MD11FSDR FDEA202510242082Hinge Bracket · corrodedLEFT WING: (ON WING SIDE), LEFT INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOTFACE AREA FOUND CORRODED. CORRODED AT LEFT HAND WING : (ON WING SIDE) , LEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE PIVOT HOLE SPOT FACE AREA REWORKED AND FOUND EXCEED LOct 24, 2025 · N603FE · Doug MD11FSDR FDEA202510242081Hinge Bracket · corrodedLEFT WING: WING SIDE LEFT INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA FOUND CORRODED. ORROSION AT LEFT HAND WING : WING SIDE LEFT HAND INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE AREA REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. ROct 24, 2025 · N603FE · Doug MD11FSDR IPXA2025112816445Skin · damagedRIGHT WING OUTBOARD MAIN FLAP L/E SKIN HAS A GOUGE AT APPROX WS 652.50. CCOMPLISHED THE PERMANENT REPAIR PER EO-95912-REQ1 AND VT-SAA EA 757-5700-01-B0636, REV. IR.Oct 23, 2025 · N409UP · Boeing 75724APFSDR SWAA2025102727874Tail Cone · crackedNUMBER 3 FLAP FAIRING BEHIND NR 1 ENGINE CRACKED. FAIRING CANOE TIP. OK TO CONTINUE PER CDL 57-10-4. SP1B NR 3 FLAP FAIRING TAIL CONE REMOVED. INSTALLED NEW TAIL CONE ASSY PER AMM 27-51-18.Oct 23, 2025 · N909WN · Boeing 7377H4SDR SWAA2025102727286Skin · delaminatedRIGHT INBD FLAP HAS SKIN DELAMINATION AT THE OTBD AFT EDGE 7" FROM EDGE OF FLAP MEASURING 3.5 LONG AND 0.5 IN WIDTH. FOUND DAMAGE TO BE IN ZONE 3 & REPAIRABLE IAW SRM 57-53-01-1A-1, REPAIRED IAW SRM 57-53-01-1A-1 (4) (A) (7) (A).Oct 23, 2025 · N440LV · Boeing 7377H4SDR IPXA2025110696806Flap · damagedRIGHT NR 1 FLAP DAMAGED, APPROX 74 INCHES FROM INBOARD EDGE AND 16 INCHES FROM TRAILING EDGE. INSTALLED REPAIR DOUBLERSEALED WITH P/N 1440B1-2AM654SK (PO/RO # SP2843294) PER EO-95513-REQ3.Oct 22, 2025 · N150UP · Airbus A300F4622RSDR DALA2025102307753Track · corrodedSHIP 3153 CORROSION ON FLAP BEARING TRACK 3 ON O/B FLAP L/H WING (1 E/A). CORRECTIVE ACTION: REPLACED FLAP BEARING TRACK #3 ON O/B FLAP L/H WING (1 E/A) AS PER A320 FAM AMM 57-52-21-000-001-A AND A320 FAM AMM 57-52-21- 400-001-A. (1266205).Oct 22, 2025 · N353NB · Airbus A319114SDR FDEA202510222070Skin · dentedREWORK: RH WING IB AFT FLAP LWR SURFACE FOUND DENT AT 58 INCHES TO OB EDGE AND 3 INCHES TO FWD EDGE. REPAIRED RH WING IB AFT FLAP LWR SURFACE DENT AT ITEF BS 279 IAW SRM 57-53-01- 2R-1, & SRM 51-70-04-2R-1, REV 51.0, EA:G-5750-T0385411 P1. MAJOR REPAIR Oct 22, 2025 · N882FD · Boeing 777F28SDR FDEA202510212061Skin · dentedDENT RH WING, LOWER SURFACE OF OUTBOARD FLAP, 36.5" OUTBOARD EDGE AND 19" TRAILING EDGE DENT RH WING, LOWER SURFACE OF OUTBOARD FLAP, 36.5'' OUTBOARD EDGE AND 19'' TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R AND SRM 57-70-10-2R REPAIR 4 FIG 201 SHOct 21, 2025 · N182FE · Boeing 7673S2FSDR SWIA2026011300018Skin · chafedRIGHT INBOARD FLAP LOWER SKIN HAS CHAFING DAMAGE AT THE INBOARD AND OUTBOARD HINGE ARM LOCATIONS FROM CONTACT WITH THE CANOE FAIRINGS. COMPLIED WITH REPAIR OF FLAP IAW REO 690-57-52-559 REV-- AND SRM 57-52-01-201-005-A01. REMOVED AND INSTALLED INNER HINGE ARMOct 18, 2025 · N548CA · Cndair CL6002D24
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