JASC 5753

Service difficulty reports · 31,506

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 DALA2024100209619Vane · dentedDENTS ON LH WING INBOARD FIXED FLAP VANE INTRADOS BETWEEN XV1=119 AND XV1=119+11, XV1=211-24, XV1=211-26. SUMMARY OF NRC 00172: DENTS (16 EA) ON LH WING INBOARD FIXED FLAP VANE INTRADOS BETWEEN XV1=119 AND XV1=119+11, XV1=211-24, AND XV1=211-26 WERE EVALUATED Sep 29, 2024 · N717JL · Boeing 717200SDR DALA2024100109592Support · corrodedSHIP 3148 CORROSION FOUND ON OUTB'D AND INB'D BORES OF PENDULUM SUPPORT ASSY AT FLAP TRACK 4 LEVEL OF OUTB'D FLAP, LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 620435-14. (0582928)Sep 29, 2024 · N348NB · Airbus A319114SDR DALA2024100109590Roller · excess playSHIP 3160 EXCESSIVE PLAY CRUISE ROLLER IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER IB FLAP ON LH WING AS PER AIRBUS CMM 57- 52-21 TASK 57-52-21-000-805-A01 AND TASK 57-52-21-400-803-A01. (0583398)Sep 29, 2024 · N360NB · Airbus A319114SDR DALA2024100309649Housing · corrodedSHIP 3148 CORROSION ON I/B FLAP BEARING HOUSING LOC. AT FLAP TRACK 3 O/B FLAP R /H WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620418-14. (0581553)Sep 28, 2024 · N348NB · Airbus A319114SDR FDEA202409281391Skin · dentedLEFT WING OUTBOARD UPPER FLAP LEADING EDGE WITH A DENT AT 12 IN. OF THE TRAILING EDGE. LEFT WING OUTBOARD UPPER FLAP LEADING EDGE AT 12" OF T/E PANEL 556AT WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 5) TABLE I AND SRM 51-70-17-0G PAR 4.H FISep 28, 2024 · N147FE · Boeing 7673S2FSDR FDEA202409281390Skin · dentedRH WING, AFT INBOARD FLAP, LOWER SKIN SURFACE, WITH DENT AT IFS 137.25, AND 12'' FROM LEADING EDGE. RH WING, AFT INBOARD FLAP, LOWER SKIN SURFACE AT IFS 137.25, AND 12'' FROM L/E WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG.201 ( SHEET 4) NOTE A AND SRSep 28, 2024 · N147FE · Boeing 7673S2FSDR FDEA202409281388Skin · dentedLEFT WING AFTER INBOARD FLAP UPPER SKIN WITH A DENT AT 3 IN. FORWARD OF THE TRAILING EDGE AND 18 IN. OF THE INBOARD EDGE LEFT WING AFTER INBOARD FLAP UPPER SKIN AT 3 IN FORWARD OF T/E AND 18 IN OF THE INBOARD EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP Sep 28, 2024 · N147FE · Boeing 7673S2FSDR FDEA202409281383Pan · erodedLH I/B MAIN FLAP OB SIDE SEAL PAN FOUND EROSION. REPAIRED LH I/B MAIN FLAP OB SIDE SEAL PAN EROSION AS PER B777 SRM 57-53-01-2R-1 AND SRM 51-70-04-2R-10 REV 47.0 AND EA G-5750-T0380710 P1, TITLE: WING-FLIGHT SURFACES-LH INBD MAIN FLAP OUTBOARD CLOSURE SEALSep 28, 2024 · N844FD · Boeing 777FHTSDR IXXA2024092805Skin · gougedLEFT WING OUTBOARD FLAP, LOWER SKIN IS GOUGED.Sep 28, 2024 · N491AZ · Boeing 767323SDR DALA2024093009558Housing · corrodedSHIP 3144 CORROSION FOUND IN TRACK 2 SUPPORT BEARING HOUSING AT RIB 9 LEVEL. CORRECTIVE ACTION: PER SECTION DTE OF 620763-14 THE REPAIR OF SECTION I IS LIMITED TO 34,300 FC FROM ACCOMPLISHMENT OF SECTION I. (0579192)Sep 27, 2024 · N344NB · Airbus A319114SDR GTIA2024093038400Fairing · damagedDURING ACCOMPLISHMENT OF OP-Z630-NKS INSPECTION FOUND R/H WING FLAP TRACK FAIRING # 631CB BROKEN/ MISSING MATERIAL. DAMAGED AREAS LENGTH 1.00IN, WIDTH N/A, AND DEPTH 0.9IN. RAF-01 3467387-01 GENERATED.-REPAIRED FLAP TRACK FAIRING 631CB ON RH WING IAW EC EA 57Sep 27, 2024 · N694NK · Airbus A320232SDR SWIA202412101303Skin · dentedRIGHT WING INBOARD FLAP, LOWER INBOARD SKIN HAS DENTS, HN00190905 (C-CHECK RO 12/8/2024) ON R/H WING I/B FLAP, REMOVED AND REPLACED DAMAGED I/B PORTION OF LOWER SKIN, REF. CRJ700 SRM 57-52-01-201-005-A01, REPAIR 005-A01. C/W 51-900-1002-SKYSep 26, 2024 · N786SK · Cndair CL6002C10SDR SWAA2024101542248Skin · delaminatedLEFT OUTBOARD AFT FLAP HAS AREA OF DELAMINATION AT LOWER O/B END<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.;[02] VERIFIED RII ITEMS COMPLETESep 26, 2024 · N952WN · Boeing 7377H4SDR DALA2024100209605Skin · delaminatedSHIP 195 FOUND RH WING I/B FLAP AFT FLAP UPPER SURFACE DELAMINATION FROM I/B END 8 INCHS AND FROM AFT END 2 INCHS. CORRECTIVE ACTION: REPAIRED RH WING I/B FLAP AFT FLAP UPPER SURFACE DELAMINATION FROM I/B END 8 INCHS AND FROM AFT END 2 INCHS AS PER B767-300 SRSep 26, 2024 · N195DN · Boeing 767332SDR DALA2024100109569Skin · scratchedSHIP 195 FOUND RH WING I/B FLAP UPPER SURFACE SCRATCH FROM I/B END 40 INCHS AND FROM AFT END 10.5 INCHS. CORRECTIVE ACTION: REPAIRED RH WING I/B FLAP AFT FLAP UPPER SURFACE SCRATCH FROM I/ B END 40 INCHS AND FROM AFT END 10.5 INCHS AS PER B767-300 SRM 57-53-01Sep 25, 2024 · N195DN · Boeing 767332SDR SWAA2024093041425Plate · damagedLH WING UPPER FIXED TRAILING EDGE WIGGLE PANEL COMMON TO 551CT; MOUNT TAB HOLES ELONGATED AND PULLED THRU.<[01] CW NDT INSPECTION OF CUTOUT REF NDT 51-00-00 PROCEDURE 23; NO DEFECTS NOTED AT THIS TIME.;[02] PERFORMED PERMANENT REPAIR ON LH WING FIXED TRAILING Sep 25, 2024 · N495WN · Boeing 7377H4SDR DALA2024092609445Roller · excess playSHIP 3144 EXCESSIVE PLAY CRUISE ROLLER IB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER IB FLAP ON RH WING AS PER AIRBUS CMM 57- 52-21 TASK 57-52-21-000-805-A01 SUBTASK 57-52-21-010-003-B01 STEP 3.B(5) AND TASK 57-52-21-400-803-A01 SUBTASK 57-52-2Sep 25, 2024 · N344NB · Airbus A319114SDR DALA2024092609444Bonding Plate · debondedSHIP 3148 DEBONDED BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 531CB AS PER ER/A 620004-14. (0575552)Sep 25, 2024 · N348NB · Airbus A319114SDR DALA2024092609443Bonding Plate · corrodedSHIP 3148 CORROSION BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. CORRECTIVE ACTION: ER/A 620004-14. (0575544)Sep 25, 2024 · N348NB · Airbus A319114SDR DALA2024092609442Bonding Plate · corrodedSHIP 3148 CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 532CB AS PER ER/A 620004-14. (0575537)Sep 25, 2024 · N348NB · Airbus A319114SDR FDEA202409241354Skin · dentedLEFT WING, OUTBOARD FLAP LOWER SURFACE WITH DENT AT 31" FROM INBOARD EDGE AND 24" FROM LOWER EDGE. LEFT WING, OUTBOARD FLAP LOWER SURFACE WITH DENT WAS REPAIRED IAW B767 SRM 57-53- 01-2R REP 1 FIG 201 (SHEET 3) AND SRM 51-70-10-2R REP 2 FIG 201 (SHEET 1) Sep 24, 2024 · N144FE · Boeing 7673S2FSDR AALA202409241287Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER EDGE. REPLACED FLAP PER AMM AMM 27-51-22.Sep 24, 2024 · N902NN · Boeing 737823SDR SWIA2024120301290Bushing · gougedLH FLAP HINGE BOX ASSEMBLY AT WS178 UPPER PRESSED BUSHINGS 4EA ARE GOUGED AND CHAFED. REQUIRES REPLACEMENT. (C-CHECK RO 11/30/2024) REMOVED AND REPLACED LH FLAP HINGE BOX ASSEMBLY AT WS178 4EA UPPER PRESSED BUSHINGS REF CRJ700 AMM 20-31-00-000-801-A01 ASep 23, 2024 · N744EV · Cndair CL6002C10SDR SWAA2024100141150Skin · cracked3/4' LONG CRACK FOUND ON RIB ;10' I/B & 2' FROM AFT SIDE OF PANEL 553BB<[01] REMOVED AND REPLACED L/H I/B TRAILING EDGE FLAP PER AMM 27-51-11 AND L/H I/B AFT FLAP PER AMM 27-51-12.Sep 23, 2024 · N409WN · Boeing 7377H4SDR DALA2024092409401Skin · dentedSHIP 3274 DISC: OUTBOARD FLAP LEFT WING ABOUT 6' FROM OUTBOARD EDGE, ABOUT 5" LONG DENT ON THE UNDERSIDE OF FLAP. C/A: PER A320 SRM 57-53 DENT MEASURES 3.90 LENGTH X 2.00' (WIDTH) X .120" DEPTH. AREA "C" NOTED TEMP REPAIR NOT REQUIRED PERMANENT REPAIR W/IN 100Sep 23, 2024 · N374NW · Airbus A320212SDR FDEA202409231338Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICSep 23, 2024 · N596FE · Doug MD11FSDR FDEA202409231337Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATSep 23, 2024 · N596FE · Doug MD11FSDR SWAA2024103040169Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL AT RH WING LOWER SURFACE 2024-592880<[01] TOOL USED CALIPER PN: 500-196-30; SN: A193117217; DUE DATE: 16/MAY/25.;[02] TOOL USED ON ITEM 2: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 2010361Sep 21, 2024 · N268WN · Boeing 7377H4SDR DALA2024092309297Bushing · corrodedSHIP 3148 CORROSION ON BUSHING (2 E/A) ON FLAP DRIVE ARM TRACK 4 ON O/B FLAP R/ H WING. CORRECTIVE ACTION: REPAIRED PER ER/A 620350-14. (0569072)Sep 21, 2024 · N348NB · Airbus A319114SDR FDEA202409201636Skin · no discrepancy00089009N00135 AIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 14~14A, T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING RSep 20, 2024 · N671FE · Airbus A300F4605RSDR SWAA2024103039886Skin · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP UPPER SURFACE IB AREA AT LT WING 2024-588315<[01] TOOL USED CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14/JAN/25.;[02] TOOL USED CALIPER P/N 500-197-30 S/N B20189443 DUE DATE 06/MAR/25;[03] TOOL USED:Sep 20, 2024 · N499WN · Boeing 7377H4SDR IPXA2024101422996Skin · dentedRIGHT WING CENTER FLAP, LEADING EDGE. DENTED FOWARD OF CENTER UPPER SKIN SLING ATTACH POINT. INSTALLED 02 EA BUTTSTRAPS AND DOUBLER TO RH CENTER FLAP LEADING EDGE SKIN. WITH RIVETS P/N: MS20426DD4-5. BATCH: 4196486. P/N: NAS1739E4-3. BATCH: 4302252 AND SEALANTSep 20, 2024 · N165UP · Airbus A300F4622RSDR DALA2024092309287Bearing · corrodedSHIP 3144 CORROSION SPHERCAL BEARING ON R/H FLAP I/B TRACK 2. CORRECTIVE ACTION: REPLACED SPHERICAL BEARING ON R/H FLAP I/B TRACK 2 AS PER A320 FAM AMM 57-52-21-000-001-A AND A320 FAM AMM 57-52-21-400-001-A. (0567208)Sep 20, 2024 · N344NB · Airbus A319114SDR SWIA20241203919Vane · chafedLH INBD FLAP VANE L/E IS CHAFED AT APPROX. WS 80 (C-CHECK RO 11/30/2024) REMOVED AND REPLACED WITH NEW LH INBD FLAP CENTER VANE AT APPX WS80 REF CRJ700 SRM 51-42-13-001-001-A01 AND DWG CC670-14010, REV -F . COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKSep 19, 2024 · N744EV · Cndair CL6002C10SDR FDEA202409191330Skin · dentedRH WING INBOARD TRAILING EDGE FLAP AFT SEGMENT LWR SKIN WITH DENTS. RH WING INBOARD TRAILING EDGE FLAP AFT SEGMENT LWR SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 (SHEET 4) NOTE A AND SRM 51-70-03-0G PAR 5.L FIG 16 REV 90 AUG 15/2024Sep 19, 2024 · N144FE · Boeing 7673S2FSDR DALA2024091909237Roller · excess playSHIP 3160 EXCESSIVE PLAY CRUISE ROLLER IB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER IB FLAP ON RH WING AS PER AIRBUS CMM 57- 52-21 TASK 57-52-21-000-805-A01 AND TASK 57-52-21-400-803-A01. (0563922)Sep 18, 2024 · N360NB · Airbus A319114SDR DALA2024091909188Bracket · crackedSHIP 3317 LHW FLAP TRACK #4 CABLE BRACKET ASSY (P/N: F5757492000600) FOUND CRACKED DURING REAR LINK INSPECTION. CORRECTIVE ACTION: R/R BRACKET PER A330 AMM 27-54. OK FOR SERVICE. (0562802)Sep 18, 2024 · N817NW · Airbus A330323SDR DALA2024091909187Bracket · crackedSHIP 3317 RHW FLAP TRACK #4 CABLE BRACKET ASSY (P/N: F5757492000700) FOUND CRACKED DURING REAR LINK INSPECTION. CORRECTIVE ACTION: R/R BRACKET PER A330 AMM 27-54. OK FOR SERVICE. (0562789)Sep 18, 2024 · N817NW · Airbus A330323SDR DALA2024091809140Hinge · excess playFREEPLAY WAS FOUND ON RH WING FLAP OUTBD HINGE AREA. SUMMARY OF NRC 00781: RH WING FLAP OUTBD HINGE WAS REPAIRED PER ER/A 620752-14 REV ORIGINAL AND PRI 620752-14 REV 2 AND WAS INSTALLED PER B717-200 AMM 27-55-03 400-801. ASSOCIATED ER/A 14-620752 ADDED FOR ACSep 17, 2024 · N989AT · Boeing 717200SDR DALA2024092609446Strut · corrodedSHIP 3144 CORROSION INTERNAL STRUCTURE OF INTERCONNECTING STRUT LH. CORRECTIVE ACTION: INSTALLED INTERCONNECTING STRUT LH ON SERVICEABLE CONDITION AND THE INSTALLATION IS TO BE ACCOMPLISHED ON AMDS CARD 2750-6020- LT. (0560270)Sep 16, 2024 · N344NB · Airbus A319114SDR DALA2024091809151Seal · wornLEFT WING #4 FLAP FAIRING (533DB) O/B AND AFT SEALS ARE WORN AWAY. FOUND DAMAGE ON TRAILING EDGE FLAP BOTTOM SIDE ( SEALS ARE ONBOARD IN FLIGHT DECK CLOSET). REMOVED PAINT , REMOVED DAMAGE PER A350-A-57-56-61-00003-664A-A(458844. REPAIRED / PREPPED AREA FOR MESep 16, 2024 · N569DZ · Airbus A350941SDR DALA2024091709080Bolt · corrodedSHIP 3133 CORROSION ON BOLT ATTACHMENT O/B FLAP TRACK 4 ON R/H WING. CORRECTIVE ACTION: REPLACED BOLT ATTACHMENT O/B FLAP TRACK 4 ON R/H WING AS PER A320 FAM AMM 27-54-62-000-001-A AND AMM 27-54-62-400-001-A. (0559847)Sep 16, 2024 · N333NB · Airbus A319114SDR DALA2024091709079Bolt · corrodedSHIP 3133 CORROSION ON BOLT ATTACHMENT O/B FLAP TRACK 3 ON R/H WING. CORRECTIVE ACTION: REPLACED BOLT ATTACHMENT O/B FLAP TRACK 3 ON R/H WING AS PER A320 FAM AMM 27-54-62-000-001-A AND AMM 27-54-62-400-001-A. (0559843)Sep 16, 2024 · N333NB · Airbus A319114SDR SWI2024F01202Fairing · chafedMX: 28845399 S/N 0137 RIGHT WING INBOARD FLAP, OUTBOARD FLAP FAIRING (686BB) HAS DONE SOME CHAFING ON FLAP. FLAGGED (C-CHECK RO 11/6/2024) PERFORMED A BLEND OUT REPAIR PER AND FOUND WITHIN LIMITS PER REO 670-57-52-568 REV -- DATED 2024-10-03 AND CRJ7Sep 14, 2024 · N787SK · Cndair CL6002C10SDR SWIA202411080914Fairing · chafedMX: 28845384 S/N 0136RIGHT WING INBOARD FLAP, INBOARD FLAP FAIRING (683BB) HAS DONE SOME CHAFING ON FLAP. FLAGGED (C-CHECK RO 11/6/2024) PERFORMED A BLEND OUT REPAIR PER AND FOUND WITHIN LIMITS PER REO 670-57-52-568 REV -- DATED 2024-10-03 AND CRJ700 SSep 14, 2024 · N787SK · Cndair CL6002C10SDR SWIA20241203912Skin · damagedADM # N744EV-8276 - L/H I/B FLAP LOWER SKIN, O/B FROM L1 FLAP HINGE FAIRING .25" I/B FROM WS 56.539 AND 4.25" FORWARD OF FLAP TRAILING EDGE. DAMAGE WITHIN LIMITS: .100L X .0800 W X .07D INCHES. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWSep 12, 2024 · N744EV · Cndair CL6002C10SDR SWAA2024093037013Skin · delaminatedRT WING O/B AFT FLAP HAS DELAMINATION ON I/B END OF UPPER SURFACE NEAR T/E.<[01] INSTALLED PANEL 643AB IAW AMM 27-51-28-400-803. 3. F. (2). BONDING CHECK GOOD.<BR>TORQUE WRENCH ID: ATS2889<BR>DUE: 05/2025<BR><BR>BONDING METER ID: ATS1257<BR>DUE DATE: 11/2024;[Sep 12, 2024 · N8652B · Boeing 7378H4SDR DALA2025040402562Hinge Fitting · damagedCORROSION AND SCRATCHES ON HOLES OF OUTBRD WING FLAP HINGE FITTING AND ON SETTLEMENT AREA OF OUTBRD WING FLAP HINGE FITTING AT LH WING. SUMMARY OF NRC 00785: CORROSION LEVEL 2. OUTBRD WING FLAP HINGE FITTING AND ON SETTLEMENT AREA OF OUTB WING FLAP HINGE FITTISep 11, 2024 · N990AT · Boeing 717200SDR SWAA2024091335844Skin · delaminatedL/H OUTBOARD AFT FLAP IS DELAMINATED ON INBD SIDE.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] C/W INSP. REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.Sep 10, 2024 · N461WN · Boeing 7377H4SDR DALA2024091108937Strut · corrodedSHIP 3148 CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON RH WING AS PER A320 FAM AMM 27 -51-44-000-001-A. (0549819)Sep 10, 2024 · N348NB · Airbus A319114
Back to JASC 5753