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 IXXA11SMN028SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP LOWER SKIN SCRATCH AND DENTS XF AT STA 174.000 TO XF 219.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 57-7-1, SDR AALA20110304TUL09Wedge · damagedFOUND DAMAGE ON TRAILING EDGE WEDGE. PREVIOUSLY MARKED. REMOVED DAMAGED CORE AND INSTALLED NEW CORE WITH AN EXTERNAL DOUBLER PER SRM 51-70-10 2R.SDR AALA20110304TUL07Skin Panel · wornRIGHT INBOARD TRAILING EDGE MAIN FLAP HAS WORN AREA 10 INCHES INBOARD END ON TOP SKIN PANEL. INSTALLED INTERIM DOUBLER PER EA 57-015596.SDR AALA20110304TUL06Flap · wornRIGHT INBOARD TRAILING EDGE MAIN FLAP, TEMP DOUBLER REPAIR ON TOP PANEL APPROXIMATELY 92 INCHES FROM OUTBOARD END. INSTALLED INTERIM DOUBLER PER EA COMP 57-015596.SDR ASAA1149157Flap · damagedRIGHT INBOARD AFT FLAP DAMAGED. TRAILING EDGE REMOVED DAMAGED FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 70 10 REPAIR 2.SDR A6WA201140180Skin · chafedLT INBD FLAP VANE L/E CHAFED AT 3 LOCATIONS. REPAIRED 3EA LOCATIONS ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-0004, REV C.SDR DALA1115859873Vane · delaminatedRIGHT WING FLAP FIXED VANE NR 2 FROM I/B HAS SOME DELAMINATION ON UPPER SURFACE AT PREVIOUS REPAIR. REPLACED RT WING FLAP NR 2 FIXED VANE WITH NEW SERVICEABLE NR 2 FIXED VANE DUE TO DELAMINATION BEING UNREPAIRABLE IAW DC9 MM 27-03 ITEM 7 FIGURE 11 SHEET 2. ISDR DALA1115849878Vane · delaminatedLEFT WING O/B FIXED FLAP VANE LOWER CENTER SURFACE DELAMINATED. REMOVED AND REPLACED LT WING OUTBD FLAP VANE TO BE INSTALLED ON WORKCARD 2750-9807M-LT VANE, FLAP, LT.SDR FDEA201103020828Rib · crackedLT WING INBD FLAP, T/E OF RIB 25A, 03 EA HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP. CRACKED RIB 25A AT LT WING INBD FLAP R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.SDR FDEA201103020827Rib · crackedRT WING INBD FLAP, T/E OF RIB 25A, 02 EA HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP. CRACKED RIB 25A AT RT WING INBD FLAP R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.SDR UALA2011030301049Bushing · faultyUNUSUAL VIBRATION WITH FLAPS FULL ON 2 CONSECUTIVE FLIGHTS. ACCOMPLISHED FLT CONT INSPECTION PAYING PARTICULAR ATTENTION TO THE FLAP NR 1 SPHERICAL BEARING LINER MIGRATION. NO DEFECTS NOTED. NO HISTORY AND POST FLT REPORT IS CLEAN. OK TO CONTINUE IN SERVICSDR FDEA201103020811Bracket · crackedRT WING OUTER FLAP T/E INBD SIDE 1 SEAL BRACKET BROKEN REPLACED DAMAGED BRACKET BY NEW BRACKET WITH RIVET REF TO SRM 51-40-21.SDR FDEA201103020810Bracket · crackedRT WING CENTER FLAP T/E OTBD SIDE 1 SEAL BRACKET BROKEN. REPLACED DAMAGE BRACKET BY NEW BRACKET WITH RIVET REF TO AB6 SRM 51-40-21.SDR FDEA201103010800Rib · crackedLT WING INBD FLAP INSP FOUND THE HORIZONTAL UPPER FLANGE OF RIB 25A IN THE UPPER FLANGE OF RIB 25A IN THE UPPER RADII CRACKED. REPLACED DAMAGED RIB BY NEW RIB WITH FASTENER REF TO EO E6-5750-7-5003 PT1 (WINGS- INBD FLAP REINFORCEMENT OF RIB 25A) REPAIR.SDR ASAA1149099Flap · damagedLT OUTBOARD FLAP OUTBOARD END DAMAGED. REPAIRED IAW B737 400 SRM 51 70 10.SDR SWAA111249Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING O/B FORE FLAP I/B LOWER CORNER SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA111235Skin · delaminatedDURING SCHEDULED 26Y CHECK, FOUND LT WING I/B MID FLAP T/E WEDGE LOWER SURFACE DELAMINATED. REPAIRED MID FLAP PER SRM.SDR SWAA111234Flap · delaminatedDURING SCHEDULED 26Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR A6WA201140247Skin · chafedRT INBD FLAP VANE L/E CHAFED 3 SPOTS. REPAIRED 3 SPOTS ON RT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C.SDR VNAA2011030300019Skin · dentedDURING SCHEDULED MAINTENANCE THE LT INBOARD FLAP SKIN WAS DENTED. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.SDR QXEA2011030200197Bracket · crackedPDX- LEFT WING NR 4 FLAP TRACK FAIRING INBOARD AFT SUPPORT BRACKET IS CRACKED. REPLACED BRACKET IAW Q400 SRM 51-42-05.SDR DALA1119311819Fairing · delaminatedLT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE WET LAY-UP REPAIR CARRIED OUT AT DELAMINTED AREA IAW SRM 51-70-03 FIG 5 AND SRM 57-53-01 REPAIR.SDR DALA1119301819Fairing · delaminatedLT WING O/B FLAP I/B EDGE L/E FAIRING FOUND DELAMINATED. COMPOSITE WET LAY-UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01 REPAIR 1 AND SRM 51-70-03 PARA 5A (1) FIG 5.SDR ASAA1149069Fitting · corrodedRT OUTBOARD FLAP OUTBOARD ROLLER GUIDE FITTING IS CHAFED. REMOVED AND REPLACED FITTING IAW B737 400 SRM 51 40 02 AND 57 51 90.SDR USAA2011032491203Skin · delaminatedSAL - S5 - DELAMINATION ON RIGHT WING OUTBOARD FLAP UPPER & LOWER SURFACES BETWEEN WS5512 TO WS6132 & BETWEEN RIB 10 TO RIB 11. REPAIRED RIGHT WING OUTBOARD FLAP UPPER & LOWER SURFACES BETWEEN WS5512 TO WS6132 & BETWEEN RIB 10 TO RIB 11 IAW A320 SRM 57-53-00 SDR DALA1119291819Skin · dentedLT WING O/B FLAP LWR SURFACE MID AREA FOUND DENT. METAL HOT BOND REPAIR PERFORMED AS PER SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 2 FIG 203.SDR SWAA111421Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA1149129Angle · chafedRT WING INBOARD FIXED TRAILING EDGE OUTBOARD ANGLE ATTACHED TO FLAP TRACK FAIRING IS CHAFED. REMOVED DAMAGED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 01 51 40 05 AND 51 40 02.SDR FDEA201102230701Skin · dentedLT WING INBD FLAP SKIN IS DENTED. BLENDED AREA NOTED; FOUND 100 PERCENT MATERIAL THICKNESS GONE IAW SRM 57-52-12, FIG 107. REMOVED DAMAGED SKIN AND REPAIRED IAW SRM 57-52-10, FIG 204 & PARA 4-D. ALODINED BARE SURFACES, SEALED DOUBLER & PRIMED IAW SRM 57-5SDR A6WA201140241Skin · chafedLT FLAP VANE L/E IS CHAFED IN 3 EA LOCATIONS. REPAIRED CHAFED ON LT FLAP VANE L/E ON 3 EA LOCATION IAW 601R-57-52-004, REV C.SDR FDEA201102220695Skin · gougedLT WING, INBD FLAP, LOWER SKIN, BEHIND GEAR GOUGED/ DENTED. REPAIRED LT WING INBD FLAP, LOWER SKIN IAW SRM 51-70-10 REPAIR IS LOCATED APPROX 5'' INBD OF FLAP TRACK FAIRING AND APPROX 6'' AFT OF L/E , FINAL REPAIR DIMENSION IS 5'' IN DIAMETER. FLAP PN 113N2003SDR FDEA201102220694Skin · delaminatedLT WING, INBD LOWER FLAP, LOWER SKIN OTBD OF CTR TRACK DELAMIATION. REPAIRED LT WING INBD LOWER FLAP, LOWER SKIN IAW SRM 51-70-17. REPAIR IS APPROX 2" OTBD OF FLAP TRACK FAIRING, AND 18" FWD OF T/E, FINAL REPAIR DIMENSION WAS 3.0" IN DIAMETER. FLAP PN : 11SDR ZZDA2011190Vane · dentedRIGHT INBOARD FIXED VANE, DENTED. ACCOMPLISHED FIXED VANE COMPOSITE REPAIR PER B717 SRM 51-70-02.SDR ZZDA2011189Vane · dentedRIGHT AFT MOVEABLE VANE, DENTED. ACCOMPLISHED MOVEABLE VANE COMPOSITE REPAIR PER B717 SRM 51-70-02.SDR V0XR201102220012Roller · corrodedFLAP ROLLERS AND PLUNGERS WORN BEYOND LIMITS. R & R (6) FLAP ROLLERS.SDR ASOA201100440Skin · dentedLT INBD FLAP LOWER SURFACE OTBD END DENTED. EVALUATED DENT ON LT OTBD FLAP LOWER SKIN BETWEEN WS 144 AND 147,3" FWD OF T/E. DENT MEASURES 2.8"X2.0X.0725", EXCEEDING ALLOWABLE DAMAGE LIMIT OF SRM 57-52-00, FIG 101, SH 2. PERFORM REPAIR IAW SRM 57-52-00. REPSDR FOTR2101903914Skin · bentPREVIOUS REPAIR ON RT WING INBD FLAP, INBD END BENT, WBL 70. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PART FROM 2024T3 .063 DIM 2.5" X 2" PO 90010689 IAW SRM 57-50-4 AND 57-50-2. INSTALLED REPAIR PART IAW SRM 51-30-2 AND 57-50-4. FASI NRSDR FDEA201102200636Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.0. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 69.0.SDR SWAA111096Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP I/B EDGE LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA111076Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED ON UPPER SURFACE I/B END. REPAIRED FORE FLAP PER SRM.SDR SWAA111836Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND DELAMINATION LT WING OUTBOARD AFT FLAP INBOARD END. REPAIRED FLAP PER SRM.SDR DALA1117820199Fairing · delaminatedLT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AS PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.SDR 2011FA0000117Structure · crackedPERFORMED INSP IAW MFG SAFETY COMUNIQUE NR 313 / FAA SAIB CE-11-21. FOUND RT FLAP L/E CRACKED (ABOUT 1.5 IN LONG) IN THE VICINITY OF THE "FLAP ACTUATOR BRACKET". FURTHER FOUND NOSE RIB CRACKED AS WELL. REMOVED FLAP FOR REPAIRS.SDR AALA20110217TUL13Skin Panel · corrodedCORROSION FOUND ON CENTER LOWER SKIN PANEL INSIDE SKIN. INSTALLED BONDED DOUBLER REPAIR PER SRM 51-70-10-2R.SDR AALA20110217TUL12Skin Panel · damagedINBOARD UPPER INTER SPAR SKIN PANEL HAS PUNCTURE ON INNER SKIN AT CENTER BAY ON OUTBOARD END. INSTALLED EXTERNAL BONDED DOUBLER PER SRM 51-70-10-2R-2.SDR AALA20110217TUL11Skin · corrodedAFT LOWER SKIN PLATE HAS CORROSION ON INBOARD RIBS. INSTALLED FABRICATED SKIN PER ESO 90399.SDR AALA20110217TUL10Rib · corrodedCORROSION AT FASTENER HOLES AND NUT PLATES ON 2 INBOARD RIBS AFT OF REAR SPAR. INSTALLED NEW RIB PER ESO 90399.SDR AALA20110217TUL09Skin Panel · damagedDENT IN LOWER SKIN PANEL 10 INCHES FROM OUTBOARD END 14 INCHES FROM TRAILING EDGE. INSTALLED FLUSH BONDED DOUBLER REPAIR PER SRM 51-70-10-2R E58-4844695.SDR AALA20110217TUL08Spar · corrodedCORROSION ON INNER SIDE OF UPPER FORWARD SPAR CHORD, 7 AND 24 TO 36 INCHES FROM INBOARD END. REPLACED UPPER FORWARD SPAR CHORD PER SRM 51-10-02 IAW ESO90399.SDR SWAA111052Wedge · puncturedDURING SCHEDULED 18Y CHECK, FOUND LT WING I/B MID FLAP T/E WEDGE LOWER SURFACE PUNCTURED. REPAIRED WEDGE PER SRM.
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