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 DL76L091902Fitting · damagedWING T/E -INBD FLAP -MAIN FLAP -COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12 AND ME13 C/W EO 01-073591-12 ME12 AND ME13.SDR DU4R2007088Torque Tube · corrodedFOUND CORROSION INSIDE RT I/B T/E FLAP FAIL/SAFE TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE ASSY P/N 113N2106-1AND I/B AND O/B CARRIAGE HALVES IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A .SDR DU4R2007087Torque Tube · corrodedFOUND CORROSION INSIDE LT I/B T/E FLAP FAIL/SAFE TORQUE TUBE. REPAIRED BY REMOVING AND REPLACING TORQUE TUBE P/N 113N2108-1 AND 2 FITTINGS I/B AND O/B IAW B757 AMM 27-51-05 AND DELTA EA 06-097981-14 REV A.SDR AWXA200700618Spar · crackedMCN - LEFT WING MID FLAP REAR SPAR UPPER CHORD CRACKED, WBL 202 - WBL 205. REPAIRED LEFT WING MID FLAP REAR SPAR UPPER CHORD, WBL 202 - WBL 205 IAW AWA ER 03-5754-07131-ES1.SDR AWXA200700574Skin · crackedMCN - MAJOR REPAIR - C-20 CHECK - RIGHT WING INBOARD MIDFLAP LEADING EDGE CRACKED, WBL 163 AT CUTOUT FOR EXHAUST GATE UPPER LINKAGE. REPAIRED RIGHT WING INBOARD MIDFLAP LEADING EDGE CRACKED, WBL 163 AT CUTOUT FOR EXHAUST GATE UPPER LINKAGE IAW B737-300 SRM 57SDR SWAA071793Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.SDR 07FDEA01398Skin · delaminatedTWO AREAS WITH DELAMINATION ON LT INBOARD FLAP BOTTOM SKIN T/E, RIB 3-5 AND RIB 8-9. REPAIR PERFORMED BY METAL SKINNED CORE REPAIR IAW SRM 57-53-12/FIG 207/209, APPROVED BY EA 6-5752-101288 AND RAS/DABRE/7006663/2006 ISSUE "A".SDR 07FDEA01386Skin · delaminatedSEVERAL DENTS WITH DELAMINATION ON RT INBOARD FLAP BOTTOM SKIN, T/E. REPAIR WAS PERFORMED IAW SRM 57-53-12/FIG 208, APPROVED BY EA 6-5752-101287 AND RAS/DABRE/7006662/2006 ISSUE "A".SDR A6WA200740210Skin · dentedBIRD STRIKE ON SHORT FINAL DENT FOUND ON LOWER LEFT INBOARD FLAP SKIN. MAINTENANCE PERFORMED A MAJOR REPAIR TO LT INBOARD FLAP LOWER SKIN BY INSTALLING A 10 INCH BY 9.25 INCH EXTERNAL REPAIR DOUBLER IAW BSC EO 601R-57-11408B. (M)SDR DL76L092045Fitting · unknownWING T/E INBD FLAP -MAIN FLAP -COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12, ME13, ME20, ME21. C/W EO 01-073591-12, ME12, ME13, ME20, ME21.SDR DL76L091893Link · damagedT/E FLAP MECHANISM 3-10 LINKS REPLACEMENT IAW 01-076248-12 ME07 LT, ME08 LT, MD09 LT AND ME10 RT ME11 RT ME12 RT. C/W EO 01-076248-12 ME07 THRU ME12.SDR DHL2007806597Skin · wornRT OTBD FLAP UPPER SKIN WORN STA XF 226.000 (MAJOR REPAIR.). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ASTAR DWG NR D857R1020 DATED 03-28-07. REMOVED EXISTING DAMAGED REPAIR SEGMENT AND INTERNAL SPLICE IAW SRM 51-1-21. FABRICATED NEW REPAIRSDR AWXA200700508Skin · debondedMCN - LEFT WING OUTBOARD FOREFLAP LOWER SURFACE DISBONDED, WBL 220 - WBL 226. REPAIRED LEFT WING OUTBOARD FOREFLAP LOWER SURFACE, WBL 220 - WBL 226 I/A/W B737-300 SRM 51-70-10-2R4 FIGURE 203.SDR CA070410004Bellcrank · cracked(CAN) LOWER LT FLAP ACTUATOR BELLCRANK SUPPORT BRACKET CRACKED AT UPPER END. WHEN FLAP IS SUBJECTED TO A SIMULATED AIR LOAD, THE SUPPORT BRACKET FLEXES AND THE CRACK VISIBLY OPENS. THIS BRACKET HAS EVIDENCE OF PREVIOUS REPAIR (A DOUBLER IS PRESENT AT THE LOWESDR SWAA071758Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR SWAA071757Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR SWAA071750Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA071738Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER AFT SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR DHL2007806518Skin · wornRT INBD FLAP UPPER SKIN WORN STA XW 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 1 ITEM D, SRM 51-1-14 PG 1. CLEANED, SDR SWAA071727Flap Track · corrodedDURING SCHEDULED 20Y CHECK, FOUND LEFT INBOARD MID FLAP OUTBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FLAP TRACK PER MM.SDR SWAA071728Flap Track · corrodedDURING SCHEDULED 20Y CHECK, FOUND LEFT INBOARD MID FLAP INBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FLAP TRACK PER MM.SDR 07FDEA01324Skin · crackedRT WING T/E DURING INSPECTION WITH EO 8-5100-7-5001 P2 FOUND 1 CRACK .25" LONG ON LOWER SKIN OF OUT'B FLAP. REPAIRED SKIN IAW SRM 57-00-01 FIGURE 4 SHT 2 VOL 1.SDR ABXA070132Hinge Fitting · crackedAFT FLAP HINGE FITTING CRACKED AT ACTUATOR ATTACH EAR, STA 164. REMOVED AND REPLACED HINGE FITTING IAW DC9 SRM.SDR 07FDEA01263Skin · dentedLT WING INB'D FLAP DENTS ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 4 VOL.1.SDR SWAA071712Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA071711Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA071726Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP PER MM.SDR SWAA071725Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP PER MM.SDR SWAA071714Flap Track · corrodedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD MID FLAP INBOARD FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FORE FLAP TRACK PER MM.SDR SWAA071713Wedge · debondedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE LOWER SKIN DISBONDED AT OUTBOARD END. REMOVED AND REPLACED T/E WEDGE PER MM.SDR 07FDEA01253Rib · crackedFOUND OLD CRACK REPAIR ON INBOARD FLAP RT, RIB 21 (POCKET REPAIR). REPAIR WAS PERFORMED BY REPLACEMENT OF RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-106443.SDR UPS07M49779Skin · dentedINSPECTION TYPE:C LEFT WING I/B FLAP UPPER SKIN, FWD OF I/B SEGMENT, FOUND WITH SEVERAL DENTS AS MARKED DENT MARK MEASURE DEP 0.015", LEN 0.90" WID 0.80", WITHIN LIMIT PER SRM 51-80-01VIIR38. HFEC INSP C/O DAC NDTSPM R13 06-10-01.001 FOUND CRACK APPX 0.5SDR 2007FA0000349Spar · looseDURING AN ANNUAL INSPECTION, THE RT FLAP IB HINGE/CONTROL BRACKET WAS FOUND TO BE LOOSE. FURTHER INSPECTION REVEALED THAT THE FLAP SPAR WAS CRACKED AT THE UPPER RIVET ATTACH POINTS. THE CRACK IS 3.5 INCH LONG AND EXTENDS PAST THE RIVET HOLES IN BOTH DIRECTIOSDR QXEA200700584Panel · chafedC3 OKC - RIGHT FLAP PANEL 684AB CHAFED ON LEADING EDGE. REPAIRED IAW SRM 57-52-01, 51-21-11.SDR QXEA200700573Skin · damagedC3 OKC - 14 EACH, LOOSE RIVETS ON UPPER SKIN OF LEFT OUTBOARD FLAP. REPAIRED IAW REO670-57-53-05.SDR SWAA071650Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR UIEA200700203Skin · delaminatedRT WING O/B MID FLAP UPPER SURFACE LEADING EDGE AT WING STA 1000.00 TO WING STA 995.00 IS DELAMINATED 2.5IN WIDE 4.5IN LONG. REPAIRED RT WING O/B MID FLAP UPPER SURFACE DELAMINATION IAW SRM 51-10-01 EO4757A353.SDR 07FDEA01210Door · wornRT IB FORE FLAP INBD UPPER HINGED LE DOOR HAS DEEP WEAR REMOVED AND REPLACED RT INBD FORE FLAP REF MM 27-51-001-4 PAGE 2. TQ WRNCH NR AAR 19624 DUE 8-19-07.SDR SWAA071614Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP UPPER AFT SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0781566Vane · gougedLEFTHAND OUTBOARD FLAP OUTBOARD VANE IS GOUGED. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0781565Vane · gougedRIGHTHAND OUTBOARD FLAP OUTBOARD VANE IS GOUGED. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0781564Doubler · gougedRIGHTHAND OUTBOARD FLAP VANE LEADING EDGE IS GOUGED AT PREVIOUS REPAIR. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0781563Doubler · chafedLEFT WING OUTBOARD FLAP CENTER VANE IS CHAFED ON EXISTING REPAIR DOUBLER. REPLACED DOUBLER PER SRM 51-70-2.SDR UPS07M50058Skin · damagedINSPECTION TYPE:C RHW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. RHW I/B FLAP LWR AFT I/B AND O/B SEGMENTS REMOVED. RHW RELATED PARTS AND I/B FLAP I/B AND O/B SEGMENTS LWR SKINS REMOVED. NEW SKINS FAB PER DWG ARC2736 AND ARC2444. NEW SKINS SDR UPS07M50046Skin · damagedINSPECTION TYPE:C LTW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. LHW I/B FLAP LWR AFT I/B AND O/B SEGMENTS REMOVED. DAMAGED SKIN REMOVED. NEW SKIN FAB PER DWG ARC2736. NEW SKIN PROTECTED, PAINTED AND INSTALLED. LHW I/B FLAP O/B SEGMENT FABSDR QXEA200700577Skin · chafedC3 OKC - LEFT INBOARD FLAP INNER SKIN CHAFED BY BONDING WIRE AT 2ND FROM INBOARD FLAP VANE GUIDE BEHIND PANEL 584BB. REPAIRED IAW SRM 51-21-11, 57-52-01.SDR SWAA071612Skin · crackedDURING SCHEDULED SPV CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP SKIN CRACKED AT INBOARD CARRIAGE ARM CUTOUT. REPAIRED FLAP PER SRM.SDR DHL2007786530Skin · gougedRIGHT WING INBD MID FLAP GOUGED 3 FROM INBD EDGE, WBL 73.597. CUTOUT DAMAGED AREA 1 BY 1.875. FABRICATED INTERNAL DOUBLER FROM 2024T3, .040, 7.75 BY 5.625 AND FILLER 2024T3, .040, 1 BY 1.875. TREATED, ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLSDR DHL2007786524Skin · dentedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF ASTAR NR 112921, LT WING OB FORE FLAP ASSY HAS 1 DENT UPPER SKIN. CUT OUT DENT 1" DIA ON LT OB FORE FLAP UPPER SURFACE AND APPLIED POTTING COMPOUND. FABRICATED FILLER 4" DIA FROM .016 2024T3 PO NR 9004174. BOSDR SWAA071593Skin · puncturedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP PUNCTURED AT LOWER SURFACE. REPAIRED FORE FLAP PER SRM.
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