JASC 5753
Service difficulty reports · 31,515
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 06FDEA2041Skin Panel · dentedFOUND LEFT WING INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS (TRAILING EDGE).SDR LR7A06055Brace · damagedDURING SCHEDULED C6 CHECK PER JOB CARD HC5712 FOUND RT INBOARD FLAP TRACK BRACE DAMAGED AT CWS 108 RT. REPLACED BRACE IAW LAC MEA 382-57-06-038.SDR LR7A06048Spar Cap · corrodedDURING SCHEDULED C6 CHECK PER JOB CARD HC5712 FOUND RT OUTBOARD FLAP LWR SPAR CAP CORRODED AT FLAP STATION 163-208. REPAIRED CAP IAW LAC MEA 382-27-06-027.SDR 06FDEA2024Structure · unknownREMOVED AND REINSTALLED SECTION INBD FLAP IAW MM 20-50-02-2. FAB PARTS IAW DETAIL PART TRAVELER N02301 AND SRM 57-10-00 FIG 4 VOL1.SDR 06FDEA2037Flap Track · corrodedFOUND CORROSION ON NR 6 FLAP TRACK AFT MOUNT PAD. REMOVED AND REPLACED NR 6 FLAP TRACK IAW TASK CARD 27X5708-03.SDR 06FDEA2028Flap Track · corrodedNR 3 FLAP TRACK UPPER SURFACE CORRODED FWD ATTACH PT OB HOLE. REMOVED AND REPLACED NR 3 FLAP TRACK IAW TASK CARD 27X5705-03.SDR SWAA061815Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM.SDR SWAA061803Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND RT WING T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA061799Skin · debondedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP T/E WEDGE DISBONDED. REPAIRED MID FLAP PER SRM.SDR SWAA061797Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING T/E OUTBOARD FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR CA060525004Bracket · cracked(CAN) DURING A BASE INSPECTION THE RT OB FLAP ACTUATOR BRACKET WAS FOUND CRACKED. WHEN THE BRACKET WAS REMOVED FROM THE SKIN, IT WAS DISCOVERED THAT THE SKIN WAS ALSO CRACKED. FURTHER INSPECTION REVEALED THAT THE RIB UNBER THE SKIN WAS ALSO DAMAGED. THE FLAP WSDR SROM200600015Torque Tube · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND NR 5 FLAP CARRIAGE OUTER TORQUE TUBE TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.SDR SROM200600013Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP REQUIREMENTS TO TRAILING EDGE FLAP CARRIAGES FOUND NR 5 CARRIAGE, INBD CARRIAGE HALF CORRODED. LEVEL 2. REMOVED AND REPLACED WITH SERVICEABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.SDR SROM200600016Torque Tube · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP INSPECTION REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 5 CARRIAGE INNER TORQUE TUBE TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICEABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.SDR SROM200600014Carriage · corrodedDURING HEAVY MAINTENANCE INSPECTION WHILE PERFORMING 10 YEAR CPCP INSPECTION REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 5 CARRIAGE OTBD CARRIAGE HALF TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCSDR AWXA200600873Bushing · missingPHX - EMERGENCY LANDING - FLT 5 - DURING TAKEOFF FROM LAS, 10 KTS BELOW V1, CREW NOTICED DEFINITE SUDDEN PULL OF RT MAIN GEAR TO THE RIGHT. DELAYED GEAR RETRACTION AND NOTICED MUCH HEAVIER THAN IN NORMAL VIBRATION. NO POPS OR BANGS REPORTED. DECLARED AN EMESDR SWAA061770Skin · debondedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP AFT LOWER INBOARD SURFACE DISBONDED. REPAIRED MID FLAP PER SRM.SDR SWAA061766Rib · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP, INBOARD RIB CORRODED. REMOVED AND REPLACED INBOARD RIB PER SRM AND CMM.SDR DHL2006873524Doubler · wornLEFT OUTBOARD FLAP UPPER SKIN DOUBLER WORN STA XF 225.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4 TR 57-94 DATED 10-01-02. REMOVED EXISTING PLATING WITH WORN REPAIR DOUBLER IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW PLASDR QXEA200601387Flap Track · corrodedPDX - C4 RIGHT HAND INBOARD FLAP TRACK NR 2 LOWER HAS DIVOTS WITH CORROSION SPOTS AT 0, 5 AND 15 DEGREE POSITIONS ON THE TOP SIDE OF THE TRACK. REPAIRED IAW RD 8-57-986.SDR QXEA200601386Flap Track · corrodedPDX - C4 RIGHT HAND INBOARD FLAP TRACK NR 2 UPPER HAS DIVOTS WITH CORROSION SPOTS AT 0 AND 5 DEGREE POSITIONS ON THE TOP AND UNDERSIDE OF THE TRACK. REPAIRED IAW RD 8-57-986.SDR SWAA061729Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING T/E AFT OUTBOARD FLAP DELAMINATED ON LOWER INBOARD SIDE. REMOVED AND REPLACED T/E AFT FLAP PER MM.SDR THMN4129SQ111Rivet · looseRT INBOARD FLAP LOWER L/E HAS 7 LOOSE RIVETS. REMOVED AND REPLACED RIVITS IAW SRM 51-30-1.SDR SIMA200614902Seal · damagedFLIGHT CREW HEARD A HUM AND FELT A HIGH FREQ VIBRATION WAS FELT SLIGHTLY IN THE RUDDER PEDALS. REPLACED RIGHT INBOARD LOWER FLAP SHROUD SEAL. REPLACED RIGHT OVERWING FAIRING NUT PLATES. REPLACED RIVETS IN RIGHT INBOARD FLAP SHROUD, AND C/W FLAP RIGGING. OPSDR SIMA200614302Seal · looseMDT - FLT 4293 - DURING CLIMB, THROUGH APPROXIMATELY FL300, CREW BEGAN TO HEAR A HUM AND FEEL A HIGH FREQUENCY VIBRATION. THE F/A AT THE SAME WAS ALSO FEELING A VIBRATION, WHICH WAS MORE NOTICEABLE IN THE REAR OF THE CABIN THAN IN THE FRONT. THE VIBRATION WASDR DHL2006873510Skin · corrodedLT INBD FLAP UPPER SKIN CORRODED (STA XW 104.000 - 115.000), MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1SDR SWAA061714Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.SDR IXXA06SMN140SSkin · damagedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND INBOARD FLAP DENTED AT SEVERAL SPOTS AND NON STANDARD REPAIR ON LOWER. SKIN BETWEEN STATIONS XW 2.000 AND XW 104.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-SDR IXXA06SMN138SSkin · dentedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF 440.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 4 TEMPORARY REVISION NUMBER 57-94 DATED 10-01-02. REMOVED DAMAGE IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-SDR IXXA06SMN139SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF 360.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 4 TR NR 57-94 DATE 10-01-02. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED NSDR UPS06247056Casting · crackedINSPECTION TYPE:C LEFT O/B FOREFLAP I/B SECTION HAS CRACKS FROM FASTENER HOLES. PAINT STRIPPED AREA IAW MM 51-20-01. HFEC INSP CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4. RESULT - CRACK CONFIRMED. FOR FLAP REPLACEMENT REF NRC 100295 DUE TO I/B CASTING NSDR QXEA200601371Skin · chafedPDX: C3. CHAFE ON UPPER SKIN ON RT OB FLAP AT YW 193.2. MAINTENANCE REPAIRED IAW Q400 NDTM PART 6, TASK 51-00-01-250-801. Q400 SRM 51-14-00, NDTM PART 1, 51-00-04 AND HORIZON EA 6-52-478.SDR MALA060344Skin · damagedRIGHT FLAP SUSTAINED DAMAGE FROM HAIL. TWO DENTS REQUIRED REPAIRS. FIRST DENT DAMAGE MEASURES 3/4 INCH IN DIAMETER AND SKIN WAS PUNCTURED LOCATED 4 3/4 INCH FROM TRAILING EDGE AND AT STATION 344.14. SECOND DENT DAMAGE MEASURES 1.0 INCH IN DIAMETER AND .011 SDR MALA060342Skin · damagedLEFT FLAP SUSTAINED DAMAGE FROM HAIL. THREE DENTS REQUIRED REPAIRS. FIRST DENT DAMAGE MEASURES 1/2 INCH IN DIAMETER AND .003 INCH IN DEPTH, LOCATED 5 1/2 INCH FROM TRAILING EDGE AND AT STATION 209.2. SECOND DENT DAMAGE MEASURE 3/8 INCH IN DIAMETER AND .003 SDR SWAA061710Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING T/E OUTBOARD AFT FLAP DELAMINATED AT OUTBOARD LOWER END. REMOVED AND REPLACED AFT FLAP PER MM.SDR MALA060333Skin · corrodedDURING 2 YEAR CHECK IN BNA FOUND CORROSION UNDER THE NR 8 FLAP CHAFE STRIP ON THE LEFT FLAP. AFTER CORROSION REMOVAL THE MATERIAL THICKNESS WAS LESS THAN THE ALLOWABLE LIMIT. A METAL BOND REPAIR WAS APPLIED IAW MESABA EO#S57060. REF: EAMS WORK ORDER 213898 TSDR DHL2006873506Skin · damagedRT OTBD FLAP EXTERNAL SKIN (UPPER) HAS AN INTERIM REPAIR AT STA XF 417.000. PERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-188745980-2 DATED 05-10-06. REMOVED PLATING WITH INTERIM REPAIR ON IT IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3SDR DHL2006873505Skin · wornLT OTBD FLAP UPPER SKIN WORN, STA XF 415.000. PERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-188745980-2 DATED 05-10-06. REMOVED WORN PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.032") IAW BOEING MESSAGE 1-188745980-2. CLEANED,SDR 06FDEA1956Flap Track · corrodedFOUND NR 2 FLAP TRACK MOUNT PAD IS CORRODED. REPLACED NR 2 FLAP TRACK ON 27X5706-03.SDR 06FDEA1949Flap Track · corrodedNR 8 FLAP TRACK IS CORRODED ON FORWARD INBOARD CLEVIS O/B FACE. REPLACED FLAP TRACK ON 27X5710-03.SDR 06FDEA1948Flap Track · corrodedNR 7 FLAP TRACK HAS CORROSION AT FWD END ON I/B CLEVIS O/B FACE. REPLACED FLAP TRACK ON 27X5709-03.SDR 06FDEA1940Wedge · crackedLT WING I/B FLAP UPPER SKIN HAS A CRACK NEAR O/B END. CLEANED AREA IAW M/M 12-22-02-7, HFEC INSP PER NTM 51-00-00 CRACK FOUND 3 EA. REMOVED T/E SECTION IAW SRM 51-31-01. REMOVED DAMAGED AREA IAW SRM 57-10-00, FIG 85. FAB DOUBLER AND FILLER MAT THICKNESS 2SDR DHL2006754518Skin · damagedLT WING IB AFT FLAP LOWER SKIN HAS TIRE DEBRIS DAMAGE. REMOVED LT WING IB FLAP IAW B727 MM 27-51-02, CUT DAMAGED SKIN DIM. 15X12.5 & VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20. FAB REPAIR SKIN DIM 15X12.5 7 2EA DOUBLER APPROX 15X 3 7075T6 .016 SDR ASAA0640593Skin · chafedLT OB FORE FLAP HAS 2 AREAS CHAFED AT IB LE. BLENDED CHAFED AREA INSTALLED RIVET IAW ASA EA 5750 02249.SDR SWAA061667Panel · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING T/E INBOARD MID FLAP WEDGE PANEL DELAMINATED. REMOVED AND REPLACED LT MID FLAP WEDGE PANEL PER MM.SDR SWAA061662Structure · wornDURING SCHEDULED C4 CHECK, FOUND RT WING T/E OUTBOARD FORE FLAP WORN AT INBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.SDR 06FDEA1925Strut · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING AFT HOLE FOUND CORRODED. LEFT HAND WING OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING AFT HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99638, TITLE: WINGS OUTBOARD TRAILING EDGE FLAP, LEFT INBOARD SDR 06FDEA1924Strut · corrodedFOUND LEFT WING OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING FORWARD HOLE FOUND CORRODED. LEFT WING OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99638. WINGS OUTBOARD TRAILING EDGE FLAP, LEFT HAND ISDR 06FDEA1923Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD FORWARD HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-99639, WINGS LT OUTBOARD TRAILING EDGE FLAP INBD BRACKET ATTACHMENT BORES CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FESDR 06FDEA1922Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING OUTBOARD AFT HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FLAP HINGE FORWARD FITTING OUTBOARD AFT HOLE CORROSION REPAIRED AS PER FEDEX E.A. NR 1-5750-99639, TITLE: WINGS LEFT OUTBOARD TR
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