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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA2023092794262Attach Fitting · corrodedINSPECTION TYPE:2CL/W A/C SIDE I/B FLAP O/B HINGE # 3 LUG O/B FACE HAS CORROSION AT REF STA. XW=254 , YW= 495.961 AND ZW=-28.941ACCOMPLISHED REPAIR IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023 , UPS EO MD11-5740-88267-A 8100-9 SIGNED BY STEPHEN KANG AR-SDR IPXA2023092794260Attach Fitting · corrodedINSPECTION TYPE:2CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG BORE HAS CORROSION AT REF STA. XW=254,YW=495.961 AND ZW=28.941ACCOMPLISHED REPAIR IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023, UPS EO MD11-5740-88267-A AND 8100-9SDR IPXA2023092794264Attach Fitting · corrodedINSPECTION TYPE:2CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT REF STA.XW=254,YW=495.961 AND ZW=-28.941REPAIR ACCOMPLISHED IAW VTSAA EA 011/5740-01-B0094 I/R DATED 09/25/2023, UPS EO. MD11-5740-88267-A DATED 09/26/2023 AND 8100-9 SIGNESDR SWAA2023103004634Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS216 AT RT WING 2023-594525<[01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE LOCATED IRSS216 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV - SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED CORRUGASDR SWAA2023101704639Flap · delaminatedLEFT WING O/B AFT FLAP I/B UPPER TRAILING EDGE TIP DELAMINATED DOT 223-LWAF2.<[01] FINAL STATEMENT: ACCOMPLISHED UT DISBOND INSP. ON UPPER SKIN AT LEFT WING O/B AFT I/B TRAILING EDGE IAW B737 NDT PART 1; 51-04-00 AND PART 4; 51-00-05. DISBOND NOTED; DAMAGE SIZSDR DXTA2023092796620Unknown · unknownFLAP SPEED EXCEEDANCE. ON A GO AROUND IN WEATHER FLAP SPEED WAS EXCEEDED BY 20 KNOTS WITH FLAP 3 DUE TO WINDS AND NOT GETTING THE FLAPS UP QUICKLY ENOUGH. LOWERED FLAPS, PERFORMED INSPECTION OF FLAPS WITH NO DEFECTS NOTED. PERFORMED SEVERAL SATISFACTORY OPS CSDR SWAA2023092604553Support Angle · crackedLEFT WING UPPER INBOARD FIXED TRAILING EDGE HAS A CRACKED SUPPORT ANGLE<[01] REMOVED AND REPLACED BRACKET REF SRM 51-40-02.SDR I5EA2023092600016Flap · damagedRH FORWARD FLAP HAS RUB DAMAGE AT LOWER O/B END OF FLAP. CUT OUT DAMAGE SECTION AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-40-02 AND B737-300 SRM 57-53-01 REPAIR 1.SDR SWAA2023103004488Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 242 AT RT WING 2023-594482<[01] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE ORSS 242 AT RT WING IAW B737-700 51-10-02 ITEM 9 AND SRM 51-40-02;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATED PLATE AND FASTENERS TSDR SWAA2023103004489Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT RT WING 2023-594479<[01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE ORSS 261 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2781 REV - SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED CORRUGATED PLATE LOCSDR SWAA2023101704304Flap · delaminatedLEFT WING OUB AFT FLAP INB END LOWER TRAILING EDGE TIP DELAMINATED MKD DOT<[01] FINAL STATEMENT: REMOVED AND REPLACED L/H O/B AFT FLAP REF AMM 27-51-22-000-81 AND 27-51-22-400-801;[02] FINAL INSPECTION; LEFT O/B AFT FLAP REPLACED.SDR SWAA2023101604297Plate · elongatedAS PER CUSTOMER REQUEST: CHECK L/H WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATES FOR CONDITION AND ELONGATED HOLES.<[01] THIS TASK WILL BE ACCOMPLISHED ON TTG8Q00NCV04;[02] VERIFIED STEP 1SDR SWAA2023110803900Retainer · crackedLEFT WING FIXED T/E DEFLECTION CONTROL RIB PANEL LOWER AFT SEAL RETAINER CRACKED AT FASTENER TAIL MKD DOT<[01] REMOVED AND REPLACED LT WING FIXED T/E DEFLECTION CONTROL RIB PANEL LOWER AFT SEAL RETAINER PER SRM 51-40-02-0G-0.;[02] VERIFIED INSTALLATION LT WINGSDR SWAA2023103003824Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 216 AT LT WING 2023-594373<[01] REPLACED CORRUGATED PLATE LOC. INBOARD TRAILING EDGE IRSS 216 AT LT WING IAW B737-700 SRM 51-10-02 AND DWG 115A2001 SHEET: 34 REV: -. SEE INDIVIDUALS SIGN-OFF BELOW;[02] REPLACEDSDR SWAA2023103003829Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 245 AT LT WING 2023-594377<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE ORSS 245 AT LT WING I.A.W B737-700 SRM 51-10-02 AND DWG 115A2001 SHEET: 32 REV: -. SEE INDIVIDUALS SIGN-OFF BELOW;[02] REPLACED CORRUGATED PLATSDR AALA202312121543Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD FLAP INTERCONNECTING STRUT AFT FITTING / BRACKET AT RIB 14. REPLACED FITTING / BRACKET PER SRM 51-72-11.SDR SWAA2023103003816Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2023-594339<[01] REPLACED ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2930 SHEET 7 REV -;[02] CERTIFIED WORSDR SWAA2023103003814Support Bracket · crackedCRACK SUPPORT BRACKET ORSS 271 TRAILING EDGE DEFLECTION CONTROL RIB AREA AT LT WING 2023-594341<[01] REPLACED SUPPORT BRACKET ORSS 271 TRAILING EDGE DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 115A2982 SHEET 4 REV.-;[02]SDR SWAA2023101910550Flap · delaminatedL/H WING ; O/B FLAP; AFT FLAP IS DELAMINATED AT I/B AFT CORNER.<[01] REMOVED L/H WING ; O/B FLAP; AFT FLAPIAW AMM 27-51-22;[02] OK TO INSTALL SERVICEABLE L/H WING ; O/B FLAP; AFT FLAP;[03] INSTALLED SERVICEABLE L/H WING ; O/B FLAP; AFT FLAP ASSY IAW AMM 27-51-SDR SWAA2023101308280Skin · debondedLEFT WING O/B AFT FLAP LOWER SKIN DISBONDED AT AFT I/B CORNER. (MARKED)<[01] THE LH OB AFT FLAP CANNOT BE REPAIRED IN A REASONABLE TIME AND IS BEING REPLACED ON FAULT TTG8Q00NLNHA.;[02] COMPLETESDR P5CA2023090600103Unknown · unknown#9 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023090600102Unknown · unknown#8 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023090600101Unknown · unknown#19 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023090600100Unknown · unknown#21 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023090500098Unknown · unknown#7 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)SDR P5CA2023090500097Unknown · unknown#6 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2023090400095Unknown · unknown#9 VC FLAP BULL NOSE O/B EDGE FOUND DELAM MARKED(<P>PERFORMED COMPOSITE WET LAYUP REPAIR AS PER SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED</P>)SDR FDEA202309211633Flap · dentedDENT ON OUTBOARD FLAP LOWER SKIN, LOCATED AT 18" FROM LOWER EDGE AND 8" FROM OUTBOARD FLAP TRACK FAIRING RH WING DENT ON OUTBOARD FLAP LOWER SKIN RH WING, LOCATED AT 18" FROM T/E AND 8" FROM OUTB FLAP TRACK FAIRING, WAS REPAIRED IAW B767 SRM 57-53-01-2R RESDR FDEA202309211630Panel · failedLH INBD UPPER FLAP TRACK CLOSE OUT PANEL (149T7760-89) DAMAGED. REPAIRED LH INBD UPPER FLAP TRACK CLOSE OUT PANEL (149T7760-89) IN REF.TO SRM 51-70-00, AND REF. EA# H-2750-T0376188 P1, STEP# 3. WO# 86959 SEQ#14.SDR SWI2023F00542Unknown · damagedRH WING OTBD FLAP HAS 1EA SMOKING RIVET ON EXTERNAL UPPER SKIN NEAR TRAILING EDGE (HN00113446) (C-CHECK RO 12/04/2023) REPAIRED RH WING OUTBD FLAP SMOKING RIVET ON EXTERNAL UPPER SKIN NEAR TRAILING EDGE REF. REO 670-57-53-337 REV-- DATED: 2023-10-07.SDR SWIA202312010001Unknown · wornMULTIPLE WEAR MARKS ALONG RH WING INBD FLAP VANE LEADING EDGE. AREAS MARKED. (HN00113442) (C-CHECK RO 12/04/2023) BLENDED OUT WEAR MARKS ON R/H FLAP VANE LEADING EDGE. REF: CRJ700 SRM 54-12-00-001-001-A01. FOUND 1 LOCATION OUT OF LIMITS. REMOVED AND INSTALSDR DALA2023092107760Unknown · unknownSHIP 3117 EXCESSIVE PLAY BEARING ON ATTACHMENT BRACKET INTERCONNECTING STRUTON INBOARD FLAP RH WING. CORRECTIVE ACTION: REPLACED ATTACHMENT BRACKET AND FASTENERS LOC ON INTERCONNECTING STRUT ON INBOARD FLAP RH WING AS PER A319 SRM 51-42-11. (2979604)SDR SWAA2023110102116Fairing · delaminatedR/W FLAP TRACK NO-6 AFT CONE FAIRING 642EB EXTERNAL SKIN APPEAR DELAMINATED<[01] SUMMARY=REMOVED FAIRING 642EB FOR ACCESS PER BOEING 737-800 SRM 51-40-02-0G-0<BR>ACCOMPLISHED TAP TEST INSPECTION IAW NDTM PART 1;51-05-01. DIS BOND NOTED. AREA MARKED (12' X 18')SDR DALA2023092607944Unknown · unknownSHIP 5806 ERA 611877-14 REV ORIGINAL SECTION I ISSUED FOR TEMPORARY REPAIR OF LOWER SKIN ON RH MAIN FLAP ASSY AT MF STA 273 AND REAR SPAR.CORRECTIVE ACTION: SECTION I WAS ACCOMPLISHED REF ERA 611877-14.SDR IPXA2023091894182Hinge Fitting · corrodedINSPECTION TYPE:2CL/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG I/B FACE HAS CORROSION AT REF. STA XW 254 , YW 495.961 AND ZW -28.941REPAIRED CORRRODED HINGE BRACKET AT THE L/H WING I/B FLAP O/B HINGE #3 I/B FACE AT STA XW 254 , YW 495.961, ZW -28.941 IAW VTSAA SDR DALA2023091807675Unknown · unknownSHIP 3117 EXCESSIVE PLAY BEARING ON DRIVE LEVER OF TRACK 2 ON RH WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY ACTUATOR DRIVE-LEVER TRACK #2 AT RH WING AS PER DWG D27550015. (2974298)SDR IPXA2023091794176Hinge Fitting · corrodedINSPECTION TYPE:2CFLAP E.O. L/H WING A/C SIDE I/B FLAP O/B HINGE #3 LUG BORE HAS CORROSIONREMOVED CORROSION AND ACCOMPLISHED EA 011-5740-01-B0093 IR, DATED 09/14/2023 AND UPS EO MD11-5740-88187-A. MINORSDR IPXA2023091794175Hinge Fitting · corrodedINSPECTION TYPE:2CL/W A/C SIDE I/B FLAP O/B HINGE #3 LUG O/B FACE HAS CORROSION.REMOVED CORROSION AND ACCOMPLISHED EA 011-5740-01-B0093 IR, DATED 09/14/2023 AND UPS EO MD11-5740-88187-A , MINORSDR FDEA202309171614Bracket · corrodedRIGHT WING WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07.OVERSIZED REPAIR BUSHING FABRICATED BSDR FDEA202309171613Bracket · corrodedLEFT WING WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07.OVERSIZED REPAIR BUSHING FABRICATED BY SDR J6BA202406100916Hinge · corrodedSIGNS OF CORROSION ON LH IB FLAP HINGE FWD ATTACHMENT HOLE AT WS80.50 (C-CHECK RO 11/16/2023) REMOVED CORROSION FROM LH INBD FWD WS 80.50.NDT PERFORMED BY BARON NDT ,LLC FAA CRS # 4NDR545D, PERFORMED ET/UT REPORT #S100423-14.PERFORMED LPI REPORT #S101923-3SDR SWIA2024053000916Hinge Fitting · corrodedSIGNS OF CORROSION ON LH IB FLAP HINGE FWD ATTACHMENT HOLE AT WS80.50 (C-CHECK RO 11/16/2023) REMOVED CORROSION FROM LH INBD FWD WS 80.50.NDT PERFORMED BY BARON NDT ,LLC FAA CRS # 4NDR545D, PERFORMED ET/UT REPORT #S100423-14.PERFORMED LPI REPORT #S101923-3SDR SWAA2023092001664Flap · lockedMOVED FLAP HANDLE TO 5; NO MOVEMENT OR FLAPS OR LEADING EDGE DEVICES; PLACED HANDLE BACK TO 0; PREPARED FOR ALTERNATE EXTENSION; AFTER PLACING FLAP HANDLE TO 5; FLAPS THE OPERATED NORMALLY<[01] PER DISCREPANCY FOLLOW FIM 27-51 TASK 836; FOUND FLAP TRANSMISSIONSDR FDEA202309161607Bracket · corrodedRIGHT WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZSDR FDEA202309161606Bracket · corrodedRIGHT WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSSDR FDEA202309161605Bracket · corrodedLEFT WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZEDSDR FDEA202309161604Bracket · corrodedLEFT WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZSDR SWAA2023102510436Flap · delaminatedR/H OUTBOARD AFT FLAP LOWER SKIN IS DELAMINATED AT THE I/B EDGE. (MARKED)<[01] VERIFIED STEP 2 IN PARTIAL.;[02] REMOVED AND REINSTALLED R/H O/B AFT FLAP IAW AMM27-51-22-400-801.;[03] REMOVED AND REPLACED R/W O/B AFT FLAP IAW AMM 27-51-22;[04] COMPLETED MEASURESDR DALA2023101308418Unknown · unknown(LOG 0011080) RH WING OUTBOARD FLAP LOWER SURFACE WITH DELAMINATION BTW WS 278.50 TO WS 302.50 FROM 1.000" TO TE AND 11.600" TO LH INNER EDGE. H WING OUTB AFT FLAP WEDGE, LOWER SURFACE AT POSITION OTEF 56.8-68, SKIN WAS REPAIRED I.A.W. B737-800 SRM 57-53-01-2RSDR SWAA2023091801622Flap · delaminatedLEFT WING OUTBOARD TRAILING EDGE AFT FLAP INBOARD SIDE SHEET METAL SKIN DISBONDED 6 INCHES IN LENGTH X 6 INCHES AT INBOARD EDGE; 3 INCHES AWAY FROM FASTENERS. (REPORTED BY PASSENGER). UPPER AFT FLAP SKIN PANEL DISBONDED<[01] REF TSR 2023007755; COMPLIED WITH E
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