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 IPXA2024022651384Skin · crackedTHE L/H CENTER FLAP ASSY HAS 1EA CRACK LOCATED ON RIB 26 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH THE PERMANENT REPAIR PER EO-89591-REQ1 AND EA 300-5750-27-A3528 REV. -.Feb 19, 2024 · N136UP · Airbus A300F4622RSDR IPXA2024022651628Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK LOCATED ON RIB 26 AFT SIDE. ACCOMPLISH PERMANENT REPAIR PER EO-89571-REQ1 AND EA 300-5750-27-A3527 REV. -. ACCOMPLISHED PERMANENT REPAIR WITH FINAL EO-89571 REQ1 AND EA# 300-5750-27-A3527. JOB COMPLETE.Feb 19, 2024 · N136UP · Airbus A300F4622RSDR IPXA2024022651656Skin · crackedTHE RT CENTER FLAP ASSY HAS 1EA CRACK LOCATED ON RIB 27 AFT SIDE. ACCOMPLISH THE PERMANENT REPAIR PER EO-89571-REQ1 AND EA 300-5750-27-A3527 REV. -. ACCOMPLISHED PERMANENT REPAIR WITH FINAL EO-89571 REQ1 AND EA# 300-5750-27-A3527. JOB COMPLETE.Feb 19, 2024 · N136UP · Airbus A300F4622RSDR FDEA202402190189Skin · chafedTHE #8 LEADING EDGE SLAT HAS A GOUGE ON THE UNDER SIDE AT WS 499. REPAIRED RH WING L/E # 8 SLAT TRAINLING EDGE WEDGE AT WS OSS 499 IN REF TO 767 SRM 57- 43-02-2R, PG 1-2 DETAIL I & III, REPAIR 1, FIG.201 SHEETS 1 & 2, AND 767 SRM 51-70-10-2R. THIS IS A MAJOFeb 19, 2024 · N190FE · Boeing 7673S2FSDR IPXA2024072139597Flap · damagedLEFT OUTBOARD FLAP DAMAGE COMPLETED MAJOR REPAIR OF LEFT OUTBOARD FLAP ON EO-89536-REQ4. ITEM REMOVED FROM DMI LOGFeb 18, 2024 · N617UP · Boeing 7478FSDR UIEA2024021000076Skin · corrodedRH WING INB AFT FLAP UPPER SKIN OUTBOARD INTERNAL DOUBLER WITH CORROSION(<P>PART WAS REPAIRED PER CMA-TLS 24-0110-04C. NO FURTHER DEFECTS NOTED.</P>)Feb 18, 2024 · N1427A · Boeing 767306SDR DALA2024021902313Strut · corrodedSHIP 3128 CORROSION CONDUIT (2EA) OF THE INTERCONNECTING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED CONDUIT (2EA) OF THE INTERCONNECTING STRUT ON LH WING AS PER AIRBUS ESPM 20-33-32-0101. (0207747)Feb 18, 2024 · N328NB · Airbus A319114SDR IPXA2025022634582Skin · damagedWHILE REMOVING LH I/B FOREFLAP, THE LEADING EDGE WAS DAMAGED NEAR O/B HINGE FITTING. 1.INSTALLED L/H WING INBD FORE FLAP TOP PANELS I.A.W SRM 51-40-02-0G REV 100 AND AMM 20-51-01-912-008 REV 110 . 2. JOB COMPLETED. REVIEW COMPELTEDFeb 17, 2024 · N575UP · Boeing 74744AFSDR AALA202402205020Support Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING IINBOARD TRAILING EDGE FLAP SUPPORT FITTING WORN ALLOWING THE BEARING TO MIGRATE ON THE OUTBOARD RIB OF THE FLAP. REPLACED SUPPORT FITTING PER SRM 51-42-11.Feb 17, 2024 · N816AW · Airbus A319132SDR FDEA202402170175Skin · crackedLH WNG CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLIGHT SURFACESFeb 17, 2024 · N653FE · Airbus A300F4605RSDR FDEA202402170174Skin · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 AND RIB15 BETWEEN STGR2.6 AND REAR SPAR. TITLE: WFeb 17, 2024 · N653FE · Airbus A300F4605RSDR FDEA202402170173Skin · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 AND RIB19 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WFeb 17, 2024 · N653FE · Airbus A300F4605RSDR FDEA202402170172Skin · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0378165 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25 AND RIB26 BETWEEN STGR2.8 AND REAR SPAR. TITLE: Feb 17, 2024 · N653FE · Airbus A300F4605RSDR FDEA202402170171Skin · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFAFeb 17, 2024 · N653FE · Airbus A300F4605RSDR FDEA202402170170Skin · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 6EA CRACKED AT RIB25,RIB26,RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB25,26,27 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WFeb 17, 2024 · N653FE · Airbus A300F4605RSDR FDEA202402170169Rib · crackedRT WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACKED AT RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB21 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES -Feb 17, 2024 · N653FE · Airbus A300F4605RSDR FDEA202402170168Rib · crackedRT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB13 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0378134 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB13 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES - RH Feb 17, 2024 · N653FE · Airbus A300F4605RSDR SWAA2024030852971Skin · delaminatedL/H OUTBOARD AFT FLAP HAS DELAMINATION ON UPPER SURFACE I/B EDGE.<[01] PARTS DATA UPDATE ONLY;[02] REMOVED AND REPLACED L/H OUTBOARD AFT FLAP PER AMM 27-51-22;[03] 2. MARK ELERY (TECHNICIAN); 22-FEB-2024 08:52 UTC<BR>REMOVED AND REPLACED L/H OUTBOARD AFT FLAP Feb 16, 2024 · N8664J · Boeing 7378H4SDR DALA2024021902314Skin · dentedSHIP 3169 DENT ON RT WING INBOARD FLAP. CORRECTIVE ACTION: REPAIRED PER ER/A 615948-14. (5040095)Feb 16, 2024 · N369NB · Airbus A319114SDR ABXA2024021900627Link · gougedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, THE RH WING OUTBD. FLAP, MAIN DRIVE LINK, SIDE LINK PIN (I I 3TI 307-8) WAS FOUND GOUGED ON THE EDGE OF THE LOWER FLANGE. THE DAMAGE WAS BLENDED PER SRM 51-10-02, WITH MATERIAL LOSS OF 0.035 INCHES. THE WIDTH OFFeb 16, 2024 · N312AA · Boeing 767223SDR COEA2024032612708Skin · chafedL/H FLAP LE CHAFING FROM INBOARD FLAP ACTUATOR ACCESS PANEL. L/H PANEL FIT INSTALLED PER C408 SRM 51-00-00 AND C408 IPC 57-20-25. L/H FLAP ACTUATOR PANELS MODIFIED AND INSTALLED IAW SR-408-ATA57-43632 REV A PARA 4.3.3 AND 4.4. OPS CHECK GOOD. NO CONTACT WITH Feb 15, 2024 · N708FX · Textrn 408SDR COEA2024032611708Access Panel · chafedR/H FLAP LE CHAFING FROM INBOARD FLAP ACTUATOR ACCESS PANEL. R/H PANEL FIT INSTALLED PER C408 SRM 51-00-00 AND C408 IPC 57-20-25. R/H FLAP ACTUATOR PANELS MODIFIED AND INSTALLED IAW SR-408-ATA57-43632 REV A PARA. 4.3.3 AND 4.4. OPS CHECK GOOD. NO CONTACT WITHFeb 15, 2024 · N708FX · Textrn 408SDR SWAA2024030652468Fairing · delaminated#1 CANOE FAIRING AFT FAIRING HAS DELAMINATION ON AFT END.<[01] REMOVED AND REPLACED #1 CANOE FAIRING AFT FAIRING IAW AIPC 27-51-28-01 AND AMM 20-50-11-910-801<BR><BR> SCREW GUN ID PER2216 CAL DUE 11/2024;[02] UPDATED PARTS FIELD;[03] VERIFIED CORRECTIVE ACTIONFeb 14, 2024 · N465WN · Boeing 7377H4SDR SWAA2024021652073Cone · delaminated#6 FLAP CANOE IS DELAMINATED ON O/B SIDE<[01] REMOVED AND REPLACED #6 FLAP CANOE AFT CONE IAW SRM 51-40-02.;[02] COMPLIED WITH INSPECTION OF THE REMOVED AND REPLACED #6 FLAP CANOE AFT CONE IAW SRM 51-40-02.Feb 14, 2024 · N278WN · Boeing 7377H4SDR DALA2024021502244Pendulum · corrodedSHIP 3124 CORROSION ON I/B FLAP PENDULUM LH WING. CORRECTIVE ACTION: PERFORMED SANDING PROCESS TO REMOVED CORROSION AS PER A319 SRM 51-74-00-801 AND SRM 51-73- 00-801. (0201567)Feb 14, 2024 · N324NB · Airbus A319114SDR DALA2024021502243Pendulum · corrodedSHIP 3124 CORROSION ON I/B FLAP PENDULUM LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 614887-14. (0201538)Feb 14, 2024 · N324NB · Airbus A319114SDR DALA2024021502240Bearing · corrodedSHIP 3124 CORROSION ON HOUSING OF FLAP BEARING LOC. TRACK 3 OF O/B FLAP R /H WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 614897-14. (0201984)Feb 14, 2024 · N324NB · Airbus A319114SDR DALA2024021402138Pendulum · corrodedSHIP 3124 CORROSION ON O/B FLAP O/B PENDULUM RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 614888-14. (0200891)Feb 14, 2024 · N324NB · Airbus A319114SDR DALA2024021402137Pendulum · corrodedSHIP 3124 CORROSION ON O/B FLAP O/B PENDULUM LH WING REFER TO AMDS CARD 2750-6020-LT. CORRECTIVE ACTION: REPAIRED PER ER/A 614884-14. (0200838)Feb 14, 2024 · N324NB · Airbus A319114SDR SWAA2024030651902Skin · crackedLEFT WING I/B AFT FLAP LOWER SURFACE HAS A CRACK 12.5' FROM T/E AND 11.5' FROM I/B EDGE.<[01] INSTALLED RAPAIR AT LEFT WING I/B AFT FLAP ON LOWER SURFACE PER SRM 51-70-10-2R-0 PARAGRAPH 20.B SIZE OF REPAIR 4' DIAMETRE VERIFIED INSTALLED RAPAIR AT LEFT WING I/BFeb 13, 2024 · N426WN · Boeing 7377H4SDR DALA2024021502242Strut · corrodedSHIP 3128 CORROSION INTERCONNECTING STRUT IB FLAP RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP RH WING ON SERVICEABLE CONDITION AS PER A320 FAM AMM 27- 51-44-000-001-A AND AS PER A320 FAM AMM 27-51-44-400-001-A. (0200614)Feb 13, 2024 · N328NB · Airbus A319114SDR DALA2024021502241Strut · corrodedSHIP 3128 CORROSION INTERCONNECTING STRUT OB FLAP LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OB FLAP LH WING ON SERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000-001-A AND AS PER A320 FAM AMM 27-51-44-000-001-A. (0200622)Feb 13, 2024 · N328NB · Airbus A319114SDR DALA2024021402140Bearing · corrodedSHIP 3128 CORROSION ON ECCENTRIC BEARING INBOARD SIDETRACK #3 OF LH WING OUTBOARD FLAP. CORRECTIVE ACTION: REPLACED ECCENTRIC BEARING INBOARD SIDE TRACK 3 ON LH WING OUTBOARD FLAP AS PER A320 FAM AMM 57-53-21-000-001-A AND A320 FAM AMM 57-53-21- 400-001-A. (02Feb 13, 2024 · N328NB · Airbus A319114SDR DALA2024021402139Bearing · excess playSHIP 3124 EXCESSIVE PLAY ON I/B FLAP O/B DRIVE ARM BEARING L/H WING. CORRECTIVE ACTION: REPLACED BRACKET BEARING ASSY ON I/B FLAP O/B DRIVE ARM BEARING L/H WING AS PER AIRBUS CMM 57-52-21-040-005-B01. (0200026)Feb 13, 2024 · N324NB · Airbus A319114SDR DALA2024021402144Bearing · corrodedSHIP 3128 CORROSION ON ECCENTRIC BEARING OUTBOARD SIDETRACK #4 OF LH WING OUTBOARD FLAP. CORRECTIVE ACTION: REPLACED ECCENTRIC BEARING OUTBOARD SIDETRACK 4 ON LH WING OUTBOARD FLAP AS PER A320 FAM AMM 57-53-21-000-001-A AND A320 FAM AMM 57-53-21- 400-001-A. (0Feb 13, 2024 · N328NB · Airbus A319114SDR AALA202403128702Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE OUTBOARD FLAP LOWER SURFACE EXTERNAL DOUBLER FOR FLAP TRACK 4. REPLACED DOUBLER PER SRM 57-53-21-300-003Feb 12, 2024 · N124US · Airbus A320214SDR AALA202402234837Bracket · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT BRACKET WORN AT RIB 14. REPLACED BRACKET PER SRM 51-42-11.Feb 12, 2024 · N807AW · Airbus A319132SDR DALA2024021302111Spar · crackedSHIP 1707 FOUND OUT LH WING IB FWD FLAP REAR SPAR UPPER CHORD CRACKED AT 25 INCHES TO IB EDGE. CORRECTIVE ACTION: LH WING I/B FWD FLAP REAR SPAR UPPER CHORD REMOVED AND REPLACED AS PER B767-800 SRM 51-40-02 (0197998)Feb 12, 2024 · N177DZ · Boeing 767332SDR DALA2024021302017Flap Track · corrodedSHIP 3124 CORROSION FOUND ON THE RH WING OUTB'D FLAP INB'D AND OUTB'D AT TRACK #3, IN THE INNER AND OUTER RIB 5 ECCENTRIC BEARING AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 614897-14. (0198762)Feb 12, 2024 · N324NB · Airbus A319114SDR VNAA2024021100019Skin · dentedHN00129326: DISCREPANCY: R/H INBOARD FLAP HAS (1EA) DENT BETWEEN F.L.S. 15.00 AND F.L.S. 24.00 NEAR TRAILIND EDGE ON LOWER SKIN. CORRECTIVE ACTION: REPAIRED DENTED LOWER SKIN IAW CRJ 900 SRM 57-52-01-201-001-A01 TYPE IV REPAIR.Feb 11, 2024 · N563NN · Cndair CL6002D24SDR 2026FA0000359Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDFeb 10, 2024 · N19NJ · Cessna 172PSDR DALA2024021201855Skin · dentedDENTS ON RH FWD MOVABLE FLAP. SUMMARY OF NRC 00381: DENTS (10 LOCATIONS) ON RH FWD MOVABLE FLAP, #2, #3, #5, #6, #8, #9, & # 10 WERE EVALUATED AND FOUND TO BE WITHIN LIMTS PER B717-200 SRM 57-53-01-1A-1 PAR 3 A (1)(2)(4). DENT #1: O/B=18 IN, T/E=6.700 IN, L=1.Feb 9, 2024 · N933AT · Boeing 717200SDR AALA202407150270Beam · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE #2 FLAP TRACK BEAM LOWER FORWARD AREA HAS CHAFE / WEAR MARKS. MAINTENANCE REPLACED THE FLAP TRACK BEAM PER AMM 57-51-33.Feb 8, 2024 · N836AW · Airbus A319132SDR DALA2024021201957Bearing · corrodedSHIP 3124 LH WING/INB FLAP/TRACK 2 BEARING AT RIB 9 LEVEL/INB & OUTB'D PLATES/ CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 31-614887. (0193526)Feb 8, 2024 · N324NB · Airbus A319114SDR SWAA2024020950088Skin · delaminatedRIGHT WING O/B TE AFT FLAP LOWER SKIN IS DELAMINATED AT LOWER I/B CORNER MEASURING 10'X10'.<[01] C/W EA 24-127-00364 (COMPONENT - SWA - REPAIR - R/H O/B T/E AFT FLAP (PN: 113A3700-28; SN: 5952) LOWER SKIN DELAMINATION - TIME LIMITED) [TTG8Q00RF14V]Feb 8, 2024 · N8693A · Boeing 7378H4SDR DALA2024020901767Flap Track · corrodedSHIP 3124 RH WING/OUTBOARD FLAP ASSY/AT FLAP TRACK #4 LEVEL/PENDULUM SUPPORT/ CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 614888-14. (0193041).Feb 8, 2024 · N324NB · Airbus A319114SDR SWAA2024030749821Angle · crackedRT WING TRAIL EDGE RIB WBL 201.90 HAS WEB AFT EDGE FITTING ANGLE CRACKED. 8-11<[01] REMOVED AND REPLACED CRACKED EDGE FITTING FROM RT WING TRAILING EDGE RIB WBL 201.90 AS PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND DWG#115A2930.;[02] VERIFIED REMOVED AND REPFeb 7, 2024 · N426WN · Boeing 7377H4SDR LR7A2024020703360Skin · crackedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB2703, FOUND LH OUTER FLAP LOWER MIDDLE SKIN CRACKED AROUND FASTENERS AT OWFS123.5L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 424825.Feb 7, 2024 · N405LC · Lkheed 382GSDR IPXA2024030630893Hinge · corrodedREPLACE L/H WING O/B FLAP O/B AFT HINGE DUE TO HEAVY CORROSION AUDIT C/W. REMOVE AND REPLACE OUTBOARD SUPPORT HINGE ASSEMBLY P/N ARC1991-501 PER CMM 57-52-04.Feb 6, 2024 · N256UP · Doug MD11FSDR IPXA2024030630467Hinge · corrodedREPLACE R/H WING O/B FLAP O/B AFT HINGE DUE TO HEAVY CORROSION REMOVE AND REPLACE OUTBOARD SUPPORT HINGE ASSEMBLY P/N ARC1991-502 PER CMM 57-52-04.Feb 6, 2024 · N256UP · Doug MD11F
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