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 ASAA0781777Skin · dentedRIGHT INBOARD FLAP INBOARD VANE HAS SEVERAL DENTS ON LOWER SURFACE. PREPARED DAMAGED SURFACE FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0781776Skin · chafedLEFT OUTBOARD FLAP VANE LEADING EDGE IS CHAFED AT INBOARD SIDE. REMOVED DAMAGED EXISTING DOUBLER. INSTALLED REPLACEMENT DOUBLER PER SRM 51-70-2.SDR ASAA0781775Skin · dentedLEFT INBOARD FLAP OUTBOARD VANE LOWER INBOARD SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA FOR BONDING. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.SDR 07FDEA02051Skin · delaminatedRT INBD FOREFLAP T/E IS DELAMINATED 36" FROM INBD END. REPAIRED DELAMINATION REF SRM 51-40-21 PG 1 AND 2, TAP TEST GOOD.SDR SWAA072786Fitting · crackedDURING SCHEDULED OTS CHECK, FOUND RIGHT WING INBOARD FORE FLAP CRACKED AT CENTER GUIDE TRACK FITTING. REMOVED AND REPLACED FORE FLAP PER MM.SDR ASAA0791772Structure · damagedRIGHT INBOARD TRAILING EDGE FLAP DAMAGE ON LEADING EDGE DUE TO SPOILER LOCKS. REPAIRED IAW EA 5750 02365.SDR ASAA0791771Structure · damagedLEFT INBOARD TRAILING EDGE FLAP DAMAGE TO THE FLAPS DUE TO SPOILER LOCKS.SDR 07FDEA02036Hinge · corrodedRIGHT WING, O/B FLAP O/B HINGE AFT FAIRING AFT STRUT FWD BOLT HOLE FOUND CORROSION. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-109897. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 2007FA0000492Bellcrank · brokenDURING ANNUAL INSPECTION, IT WAS NOTED THAT THE (BELLCRANK ASSY) ON THE FLAP FEEDBACK LEVER, BEHIND THE INSTRUMENT PANEL, WAS BROKEN IN TWO, IT CONSIST OF A PLASTIC BLOCK WITH A SLOT IN IT WHICH MOVES THE MICROSWITCH ASSY TO ACTIVATE, OR DEACTIVATE THE FLAP DRSDR QXEA200700921Panel · chafedC1 OKC - LEFT FLAP PANEL 584AB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 51-12-00 AND 51-21-11.SDR QXEA200700920Panel · chafedC1 OKC - LEFT FLAP PANEL 584EB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11.SDR SWAA072741Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR QXEA200700915Panel · chafedCI OKC - FLAP PANEL 684HT UPPER LEADING EDGE DAMAGED. REPAIRED IAW SRM 51-12-00, 51-21-11.SDR QXEA200700919Panel · chafedC1 OKC - RIGHT FLAP PANEL 684GB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11.SDR QXEA200700918Panel · chafedC1 OKC - RIGHT FLAP PANEL 684JB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11.SDR QXEA200700917Panel · chafedC1 OKC - RIGHT FLAP PANEL 684LB CHAFED. REPAIRED IAW SRM 51-12-00 AND 51-21-11.SDR QXEA200700916Panel · chafedC1 OKC - RIGHT FLAP PANEL 684DB CHAFED. REPAIRED IAW SRM 51-2-00 AND 51-21-11.SDR QXEA200700895Web · damagedC4 PDX - RIGHT WING FLAP SHROUD WEB HAS DAMAGE ON LIGHTENING HOLE APPEAR TO BE FROM SPOILER ACTUATOR LINK. TOGGLE AT STATION YW 317.019. REPAIRED IAW RD8/4-57-158.SDR SWAA072730Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR ASAA0741702Skin · delaminatedLEFT WING O/B TRAILING EDGE FLAP IS DELAMINATED AT I/B AFT CORNER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.SDR 2007UALA01668Skin · crackedRIGHT WING INBOARD TRAILING EDGE FOREFLAP LOWER SURFACE CRACKED. REPAIRED WITH WET LAYUP AND BMS8-301 RESIN PER UA-EVA-70288 AND BOEING TELEX 8100-9. SUSPECT INSTALATION & RIG CAUSED UNUSUAL DYNAMIC LOADING DURING FLIGHT.SDR 07FDEA01991Hinge Fitting · crackedRIGHT WING, O/B FLAP I/B HINGE FITTING FOUND CRACK AT STA XOF 556. [06-18-07] RIGHT WING - O/B FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00-5, FOUND SATIS.SDR SWAA072688Flap · debondedDURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD MID FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.SDR QXEA200700884Skin · chafedC4 PDX - THE LEFT OUTBOARD FLAP UPPER SURFACE IS CHAFED ABOUT 2" FROM THE INBOARD END. REPAIRED IAW SRM 57-52-30, RD8/4-57-809.SDR QXEA200700883Skin · chafedC4 PDX - THE LEFT INBOARD FLAP UPPER SURFACE HAS CHAFE INTO THE SKIN 6" FROM THE INBOARD END. REPAIRED IAW SRM 57-51-30, RD8/4-57-807.SDR AMTA200700245Skin · dentedRT IB FLAP TRAILING WEDGE SECTION NUMEROUS NICKS AND DENTS ON LOWER SKIN. REPAIRED IAW EA 737-5753-09-A0858. (K)SDR DLM88070593Skin · damagedTHE RHS INBOARD FLAP REMOVALBE PANEL LOWER SKIN REQUIRED A SKIN SPLICE PER 461910-14.SDR DHL2007740509Skin · delaminatedRT O/B AFT FLAP WBL 417 HAS DELAMINATION AND SURFACE CORROSION ON AN NEAR T/E. REMOVED DAMAGED AREA APPROX 10" BY 20". CLEANED AN PREPPED AREA TO BE REPAIRED. FAB`D FILLER 10" BY 20" AN 2 DOUBLERS 3" BY 20" FROM .016" 2024-T3 PO NR 9004174. ANODIZED AN PRISDR DHL2007803504Skin · wornRT OUTBD FLAP UPPER SKIN WORN STA XF 207.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR NR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 4, TRSDR DLM88070596Vane · delaminatedINAPPROPRIATE REPAIR AND DELAMINATION WERE REPAIRED TO A LT WING OUTBD FLAP CENTER FIXED GUIDE VANE, NEAR THE INBD END. REPAIR INCLUDED A 16" WIDE SKIN SPLICE, AND A SECOND 11" WIDE DOUBLER. THE REPAIR IS PERMANENT.SDR SWAA072632Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA072637Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR ASAA0741695Skin · dentedRIGHT WING O/B FORE FLAP DENTED ON UPPER SURFACE. DENT REPAIRED IAW SRM 51-70-10 REPAIR 4.SDR SROM200700003Bearing · looseAIRFRAME BUFFET NOTED AFTER GEAR UP ON TAKEOFF & BEFORE FLAP RETRACTION & POWER REDUCTION DURING CLIMB. THIS IS THE 2ND WRITE UP OF THIS CONDITION. PERFORMED AIRFRAME CONDITIONAL INSPECTION. REPLACED NLG GRAVEL SKI DEFLECTOR ACTUATOR DUE TO LOOSE ROD END ANSDR SWAA072606Skin · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR 07FDEA01881Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE OF INBOARD FLAP WS 339-409 RIB 6-7. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM SDR 07FDEA01905Flap · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RT LOWER WING SURFACE OF OUTBOARD FLAP WS 874-935 RIB 14-15. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE JASC/ATA CODE INDICATED SHOULD BE 5750. RESDR 07FDEA01899Flap · delaminatedPREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF OUTBOARD FLAP WS 663-737 RIB 11-12. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE PRESENT SDR CONCERNS THE SAME NR AS SDSDR 07FDEA01897Flap · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE T/E OF INBOARD FLAP WS0-67 RIB 1-2. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE PRESENT SDR CONCERNS THE SAME NR AS SDR 07-220SDR 07FDEA01882Flap · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF OUTBOARD FLAP WS 874-935 RIB 14-15. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO ANSDR 07FDEA01883Flap · nonePREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE OUTBOARD FLAP WS935-996 RIB15-16. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX ENGINEERING AUTHORIZATSDR SWAA072559Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.SDR SWAA072558Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.SDR ASAA0741655Skin · dentedLEFT WING O/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-10.SDR SWAA072525Attach Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 1 FLAP TRACK AFT ATTACH FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER SRM AND BOEING DRAWING.SDR 07FDEA01853Flap Track · wornLT WING TE IB FLAP OB TRACK UPP OB FLG WEAR STEP HAS GOUGES/ HIGH METAL 5" - 32" FROM AFT END. LT WING INBD T/E FLAP OUTBD (NR 3) FLAP TRACK REPLACED ON W/C 27X5705-03.SDR 07FDEA01851Flap Track · corrodedRT WING TOP SIDE OF I/B FLAP O/B FLAP TRACK AT MOUNT HOLE IS CORRODED RT I/B FLAP TRACK (NR 6) REPLACED. NEW TRACK INSTALLED ON W/C 27X5708-03.SDR DHL2007785001Skin · chafedWHILE IN "A" CHECK, RT INBD TE FLAP PREVIOUS REPAIR HAS CHAFFING ON LE OF FOREFLAP. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 2024T3 .063 PO NR 9005138 DIM 5 1/4" BY 4 1/4' IAW B727 SRM 57-50-04 FIG 1 AND 57-50-2 FIG 3. TREATSDR SWAA072507Flap · crackedDURING SCHEDULED BRDG CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP CRACKED. REPAIRED FLAP PER SRM.SDR 07FDEA01847Skin · delaminatedFOUND REPAIR LOCATED AT RT O/B FOREFLAP LWR SURFACE I/B END ON AGING A/C INSP. EXISTING REPAIR DID NOT CONFORM TO CURRENT SRM 51-40-20. REPAIRED RT O/B FOREFLAP AREA REF SRM 51-40-20 PARA 14-20, 21, 22.
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