JASC 5753

Service difficulty reports · 31,513

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 JJBA20240325090Angle · corrodedRH IB FLAP IB ANGLE CORRODED. OLD ANGLE REMOVED, NEW ANGLE PARTIALLY INSTALLED. INSTALLATION OF NEW BRACKET COMPLETEDMar 6, 2024 · N16183 · Emb EMB145XRSDR SWAA2024031159732Fairing · pulled# FLAP TRACK FAIRING AFT CONE HAS 3 EA PULLED FASTENERS ON OUTBD SIDE<[01] REMOVED AND REPLACED #3 FLAP TRACK FAIRING AFT CONE REF AMM 27-51-18Mar 6, 2024 · N8310C · Boeing 7378H4SDR JGVR20240306001Skin · corrodedBLENDED CORRODED AREAS UNDER THE NUTPLATES COMMON TO THE LH & RH WING FLAP PANELS 523AB AND 623AB, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH NETJETS RFTS-110102.Mar 6, 2024 · N317QS · Cessna 680CESDR DALA2024030603059Roller · wornSHIP 3418 LEFT WING O/B FLAP, O/B ROLLER WORN. CORRECTIVE ACTION: REMOVED AND REPLACED ROLLER W/REF A330 AMM 27-54-73. OK FOR SERVICE. (0232284)Mar 6, 2024 · N418DX · Airbus A330941SDR SWAA2024041159046Fairing · damagedRIGHT NR 6 FLAP TRACK AFT FAIRING WITH ELONGATED HOLES AT OB MID SEAL INSTALLATION. REPAIRED DAMAGE AND RESTORED AREA AT NR 6 FLAP TRACK FAIRING O/B MID SEAL AREA IAW SRM 51-70-04-2R-9.Mar 5, 2024 · N8321D · Boeing 7378H4SDR SWAA2024041159047Fairing · damagedLEFT NR 3 FLAP TRACK AFT FAIRING WITH ELONGATED HOLES AT OB MID SEAL INSTALLATION. REPAIRED DAMAGE AND RESTORED AREA AT #3 FLAP TRACK FAIRING AS PER SRM51-70-04-2R-9.Mar 5, 2024 · N8321D · Boeing 7378H4SDR SWAA2024041159612Skin · delaminatedLEFT WING OTBD AFT FLAP INBD T/E LOWER SURFACE AREA DELAMINATED. REMOVED AND REPLACED LT WING OTBD FLAP AFT FLAP AND ALSO ACCOMPLISHED ADJUSTMENT IAW AMM 27-51-22-400-801,Mar 5, 2024 · N8321D · Boeing 7378H4SDR SWAA2024041159616Skin · delaminatedRIGHT WING OTBD AFT FLAP INBD LOWER T/E AREA DELAMINATED. REMOVED AND REPLACED R/H WING O/B FLAP AFT FLAP AND ALSO ACCOMPLISHED ADJUSTMENT AS PER AMM 27-51-22-401-NG.Mar 5, 2024 · N8321D · Boeing 7378H4SDR JJBA20240318068Angle · corrodedLH OB FLAP IB ANGLE CORRODED. AT LH OB FLAP, ANGLE BRACKET REMOVED FOR REPLACEMENT. CORROSION FOUND ON BRACKET OUTBOARD FLAP WING BLENDED. NEW LH OB ANGLE INSTALLEDMar 5, 2024 · N16183 · Emb EMB145XRSDR IPXA2024030479473Skin · damaged*SDR FILED OPEN* L/W INBD UPPER FLAP UPPER SURFACE SKIN DAMAGE FOUND ADDITIONAL DAMAGE TO INNER SKIN AT REPAIR LOCATION. STOP DRILLS THRU LOWER SKIN AT TWO LOCATIONS. PARTIALLY REMOVED LOWER FLAP SKIN FOR ACCESS.Mar 4, 2024 · N338UP · Boeing 76734AFSDR ASAA2024030448792Skin · dentedLESSOR ITEM 767 RH WING TRAILING EDGE IB FLAP LOWER SURFACE I/B CLUSTER OF DENTS REQUIRES REPAIR. GROUNDED - YES. REPAIRED RH WING TRAILING EDGE IB FLAP LOWER SURFACE I/B CLUSTER. FINAL DIMENSIONS OF REPAIR ARE 12.5"W X 11.8"L LOCATED 47.5" FROM INBRD AND STOPMar 4, 2024 · N847VA · Airbus A320214SDR DALA2025103107962Vane · corrodedCORROSION ON LOWER SKIN OF OUTBD FLAP VANE AT RT WING. OTBD FLAP VANE AT RT WING WAS REPLACED BY ONE SERVICEABLE OTBD FLAP VANE (0228760).Mar 3, 2024 · N982AT · Boeing 717200SDR SWAA2024040958576Panel · debondedDEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE O/B SIDE AT RT WING. REPAIRED IB MAIN FLAP WEDGE PANEL LOWER SURFACE O/B SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-7 REPAIR 7.Mar 3, 2024 · N247WN · Boeing 7377H4SDR UIEA2024022600130Skin · delaminatedRHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)Mar 3, 2024 · N454PA · Boeing 74746NFSDR UIEA2024022600131Skin · delaminatedLHW O/B FORE FLAP FOUND  DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)Mar 3, 2024 · N454PA · Boeing 74746NFSDR UIEA2024022600132Skin · delaminatedLHW O/B FORE FLAP FOUND  DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Mar 3, 2024 · N454PA · Boeing 74746NFSDR UIEA2024022600133Skin · delaminatedRHW I/B AFT FLAP FOUND DELAMINATION. PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)Mar 3, 2024 · N454PA · Boeing 74746NFSDR SWI202405080360Vane · chafedRIGHT INBOARD FLAP, FLAP VANE. LEADING EDGE AT FLS72 IS CHAFED. (MARKED) (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED 1EA NEW R/H INBD FLAP VANE CAP AT FLS72 PER CRJ700SRM 51-42-13-001-001-A01 AND CRJ700SRM 51-23-00-001-001-A01 AND DWG CC670-14010 REV -F. SMar 2, 2024 · N730EV · Cndair CL6002C10SDR SWIA202405080302Skin · damagedLEFT INBOARD FLAP LOWER SKIN HAS A CREASE FLS 41 AND 5.5 INCHES FROM THE TRAILING EDGE. (MARKED) (C-CHECK RO 5/6/2024) L/H I/B FLAP LOWER SKIN HAS BEEN REPAIRED REF CRJ SRM 57-52-01-201-002-A01, TYPE 4, PERMANENT NON FLUSH REPAIR.. COMPLIED FULLY W/SKYCAMar 2, 2024 · N730EV · Cndair CL6002C10SDR AALA202404296468Skin · debondedAIRCRAFT WAS GROUNDED: LEFT WING TRAILING EDGE OUTBOARD FLAP TRAILING EDGE LOWER SURFACE EXTERNAL BONDED REPAIR HAS BECOME DISBONDED AND STARTING TO FAIL 66 INCHES FROM THE INBOARD EDGE. MAINTENANCE REPLACED THE FLAP ASSEMBLY PER TASK CARD 26L00027009.Mar 2, 2024 · N703UW · Airbus A319112SDR JR2R20240427728Skin · crushedRH O/B FLAP FAIRING 633BB CRUSHED RH O/B AFT FLAP SKINMar 2, 2024 · N85320 · Emb ERJ170200LRSDR AALA202403086468Skin · debondedAIRCRAFT WAS GROUNDED: LEFT WING TRAILING EDGE OUTBOARD FLAP TRAILING EDGE LOWER SURFACE EXTERNAL BONDED REPAIR HAS BECOME DISBONDED AND STARTING TO FAIL 66 INCHES FROM THE INBOARD EDGE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)Mar 2, 2024 · N703UW · Airbus A319112SDR DALA2024030402977Bonding Plate · damagedSHIP 3128 DAMAGED BONDING PLATE FLAP TRACK FAIRING 631CB ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 615323-14. (0226234)Mar 2, 2024 · N328NB · Airbus A319114SDR DALA2024030402976Bonding Plate · damagedSHIP 3128 DEBONDED BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 615323-14. (0226204)Mar 2, 2024 · N328NB · Airbus A319114SDR DALA2024030402975Bonding Plate · damagedSHIP 3128 DAMAGED BONDING PLATES WERE FOUND AT FLAP TRACK #2. CORRECTIVE ACTION: REPAIRED PER ER/A 615323-14. (0226196)Mar 2, 2024 · N328NB · Airbus A319114SDR SWAA2024030557869Retainer · crackedAFT UPPER TRAILING EDGE SEAL RETAINER JUST O/B OF THE #3 FLAP TRACK IS CRACKED<[01] REMOVED AND REPLACED SEAL RETAINER FITTING IAW SRM 51-40-02.;[02] C/W INSPECTIONMar 1, 2024 · N7813P · Boeing 7377K9SDR YENA2024030500330Skin · debondedDURING HEAVY MAINTENANCE: DEBONDED OB FLAP SURFACE ON RH WING; REPAIRED OB FLAP LOWER SURFACE ON RH WING IAW EC# A24-129-01, EA# 57-0022-24 REVISION 0 AND EA# 57-0022-24 PART 1. TOOL USED: DIGITAL CALIPER: P/N 500-197-30, S/N A21043111, DUE DATE: JUL/20/2024. Mar 1, 2024 · N536JB · Airbus A320232SDR IPXA2024040823808Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 12 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. EMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED NEW REPAIR FLANFeb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040823096Skin · crackedTHE L/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 26 FWD. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGE AT CENTER FLAP RIB 26 BETWEEN STR 2.6 TO STR 2.7 AND FABRICATED NEW REPAIR ANGLE WITH MATERIAL 2024-T3 .056C. TRFeb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040825603Skin · crackedTHE R/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 27 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGE AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066 IN ACCOMPLISH WITH STEP 58 ON EAFeb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040825406Skin · crackedTHE R/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 26 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. ACCOMPLISH PERMANENT REPAIR PER EO-89700-REQ1 AND EA 300-5750-27-A3537.Feb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040825155Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 25 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. TREATED AND PRIMED NEW REPAIR DOUBLER IAW A300-600 SRM 51-21-10. NSTALLED NEW DOUBLER IN ACCOMPLISH WITH STED 69 ON EA 300-5750-27-A353Feb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040824763Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 18 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED IAW A300-600 SFeb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040824243Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 17 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED NEW REPAIR FLAFeb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040824047Skin · crackedHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 13 AFT. ON THE UPPER SURFACE. ACCOMPLISH PERMANENT REPAIR PER EO-89700-REQ1 AND EA 300-5750-27-A3537 REV. -.Feb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040823430Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 11 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. FABRICATED NEW REPAIR FLANGE AND NEW REPAIR STIFFENER WITH MATERIAL 2024-T3 .050C BATCH 0004247654 IN ACCOMPLISH WITH STEP 6 ON EA 300-Feb 29, 2024 · N158UP · Airbus A300F4622RSDR IPXA2024040822772Skin · crackedTHE L/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 26 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGES AT CENTER FLAP RIB 26 BTW STR 2.7 TO REAR SPAR AND FABRICATED 02 EA NEW REPAIR ANGLES WITH MATERIAL 2024-T3 .Feb 29, 2024 · N158UP · Airbus A300F4622RSDR SWAA2024031557167Skin · delaminatedLH WING O/B TRAILING EDGE FLAP UPPER SURFACE DELAMINATED APPROXIMATELY 6.5' X 4.0' LOCATED AT 1.5' FROM I/B END AND 1.5' FROM TRAILING EDGE. T/E AFT FLAP (LH OTBD) (PN: 113A3700-25 SN: S1401-10)<[01] REMOVED L/H WING O/B AFT FLAP PER AMM 27-51-22.;[02] INSTALLFeb 28, 2024 · N8624J · Boeing 7378H4SDR SWAA2024040356902Skin · delaminatedSKIN DELAMINATION ON L/H O/B AFT FLAP LOWER SURFACE 1.7' TO 3.0' FROM I/B END; 4.5' TO 11.0' FROM T/E.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801Feb 27, 2024 · N460WN · Boeing 7377H4SDR SWAA2024031556543Skin · delaminatedLH INBD MAIN FLAP OUTBD TRAILING EDGE WEDGE DELAMINATED ON LOWER SURFACE<[01] LOCATED AND DRILLED LH INBD MAIN FLAP OUTBD TRAILING EDGE WEDGE PER SRM 51-40-02;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMFeb 27, 2024 · N8624J · Boeing 7378H4SDR R61A2024031000106Fitting · crackedSUSPECTED CRACK IB AFT FLAP, IB SIDE EMITING FROM BOLT. REQUIRED NDT TO CONFIRM. FITTING (R/H IB AFT FLAP- IB SIDE) REPLACED IAW EMBRAER 170/175 AMM 20-10-01-910-801-A TABLE 201 AND 203 AND SRM 51-21-05.Feb 26, 2024 · N860RW · Emb ERJ170100SESDR FDEA202402260216Skin · delaminatedLEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 190 AND OTEF STA 265.69 WITH DELAMINATION. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 190 AND OTEF STA 265.69 WAS REPAIRED IAW B767Feb 26, 2024 · N160FE · Boeing 7673S2FSDR FDEA202402260215Skin · delaminatedLEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 3.75 AND OTEF STA 83.73 WITH DELAMINATION. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 3.75 AND OTEF STA 83.73 WAS REPAIRED IAW B767Feb 26, 2024 · N160FE · Boeing 7673S2FSDR SWIA202404250316Skin · buckledLEFT WING OUTBOARD FLAP LOWER SIDE SKIN APPROXIMATELY FLS209 BUCKLING , HN00140933 (C-CHECK RO 4/24/2024) LEFT WING OUTBOARD FLAP LOWER SIDE SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3, PERMANENT NON FLUSH REPAIR. REFER TO CONTIFeb 23, 2024 · N753SK · Cndair CL6002C10SDR SWI202404250316Skin · buckledLEFT WING OUTBOARD FLAP LOWER SIDE SKIN APPROXIMATELY FLS209 BUCKLING , HN00140933 (C-CHECK RO 4/24/2024) LEFT WING OUTBOARD FLAP LOWER SIDE SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3, PERMANENT NON FLUSH REPAIR. REFER TO CONTIFeb 23, 2024 · N753SK · Cndair CL6002C10SDR UIEA2024021500088Skin · delaminatedRH WING OUTBOARD FLAP LOWER SKIN EXISTING REPAIR WITH DELAMINATION (23 IN FROM L/E & 48 IN FROM LH EDGE)(<P>RH WING OUTBOARD FLAP LOWER SKIN PANEL WAS REPAIRED PER SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED.</P>)Feb 22, 2024 · N663GT · Boeing 767324SDR IXXA2024022202Skin · corrodedLEFT WING IB FLAP HAS CORROSION ON UPPER SURFACE.Feb 22, 2024 · N431AZ · Boeing 767381SDR SWIA2024032500221Skin · damagedRIGHT OUTBOARD FLAP HAS SMOKING RIVITS ON THE OUTTER SKIN (C-CHECK RO 3/23/2024) REMOVED AND REPLACED 10EA SMOKING FASTENERS ON RH OUTBOARD FLAP PER MHIRJ REO 670-57-53-347, REV: --, DATED 2024-02-24. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY.SKYCAFeb 21, 2024 · N744SK · Cndair CL6002C10SDR 2026FA0000337Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF ON THE INBOARD LH FLAP TRACKFeb 20, 2024 · N543ND · Cessna 172SSDR REXA2024102901114Access Panel · chafedRH FLAP L/E ACCESS PANEL 684GB IS CHAFED. FOUND DAMAGE ON PANEL BEYOND REPAIR. LOCATED AND DRILLED NEW SERVICABLE PANEL 684GB IAW CRJ-900 SRM 51-40-11-001-001-A01.Feb 19, 2024 · N303PQ · Cndair CL6002D24
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