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 ASAA1047344Flap Track · chafedLEFT O/B FLAP AFT FLAP TRACK FROM O/B END AREA OF MID FLAP SKIN CHAFED. REPAIRED BY INSTALLING DOUBLERS.SDR FOTR20006NR1992Skin · dentedRT WING INBD FLAP LOWER SURFACE IS DENTED AT WS 135. REPAIRED ON FASI W/O 20006, N/R 01992, INSTALLED HOT BONDED REPAIR TO LOWER SURFACE OF RT INBD AFT FLAP AT WS 135 IAW SRM 51-40-20 PARA 7, PARA 8 AND PARA 20, REV 102. MATERIAL USED: 7075-T6, 0.016". DIM; FSDR FOTR20006NR1850Structure · puncturedRT INBD AFT FLAP LOWER SURFACE IS PUNCTURED NEAR INBD END. REPAIRED ON FASI W/O NR 20006, NR 01850. INSTALLED HOT BONDED REPAIR TO RIGHT INBD AFT FLAP LOWER SURFACE AT WBL 75 IAW B727 SRM 51-40-20 PARA 20, REV 102. MATERIAL USED: 2024-T3, 0.012 THICK, 3 DIASDR SWAA100691Rib · crackedDURING SCHEDULED 14Y CHECK, FOUND RT WING I/B MID FLAP I/B AFT RIB CRACKED. REMOVED AND REPLACED RIB PER SRM.SDR SWAA100680Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA100665Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA100656Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA100641Flap · delaminatedDURING SCHEDULED 8Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR FOTR20006NR1795Skin · crackedLT OTBD FOREFLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O NR 20006,NR 01795 - INSTALLED REPAIR DOUBLER TO LT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-4 FIG 7 REV 102. MATERIAL USED: 2024-T3, DIM.; 6 X 4 X 0.063.SDR FOTR20006NR1794Skin · crackedRT OTBD FORE FLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O 20006, NR 01794. INSTALLED REPAIR DOUBLER TO RT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-2, FIG 4 AND 57-50-4 FIG 1 REV 102. MATERIAL USED: 2024-T3, DIM.; 5 X 3 X 0.063.SDR SWAA100660Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR A6WA201040180Attach Bracket · crackedLT WING BUTE 594JB ATTACH BRACKET BROKEN. REMOVED BROKEN BRACKET & REPLACED WITH NEW BRACKET PN 600-10196-15.SDR SWIA201023599Panel · defectiveUNCOMMANDED ROLL WITH FLAPS EXTENDED TO 45°. (FLT 1002) REPLACED FLAP PANEL.SDR FOTR20006NR5046Skin · delaminatedRT WING OTBD AFT FLAP IS DELAMINATED STA WBL 348. REPAIRED ON FASI WO 20006, N/R 05046. REPAIRED RT WING OTBD AFT FLAP AT WBL 348.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.012, DIM: 2.0 BY 6.0, FILLER; 7075-TSDR FOTR20006NR5049Skin · gougedRT WING INBD FORE FLAP OB LOWER SKIN IS GOUGED. REPAIRED ON FASI WO 20006. N/R 05049- REPAIRED RT WING INBD FORE FLAP OTBD LOWER SKIN AT STA 240.0 IAW SRM 57-50-4 FIG 1, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.063", DIM: 5.250" X 4.125".SDR FOTR20006NR5051Skin · delaminatedRT WING INBD AFT FLAP UPPER SURFACE IS DELAMINATED STA130. REPAIRED ON FASI WO 20006, N/R 05051. REPAIRED RT WING INBD AFT FLAP UPPER SURFACE AT WBL 130.0 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.016, DIM: 14.SDR FOTR20006NR5050Skin · damagedRT WING AFT IB FLAP LOWER SURFACE HAS GRAVEL DAMAGE AT INBD END. REPAIRED ON FASI WO 20006. N/R 05050- REPAIRED RT WING AFT INBD FLAP LOWER SURFACE AT WBL 115.0 BY HOT BONDING REPAIR IAW SRM 51-40-20 AND 57-50-2 FIG 3, REV 102. MATERIAL USED: DOUBLER- 7075-T6SDR FOTR20006NR5170Angle · crackedLT IB MIDFLAP LOWER AFT CLOSE OUT CHORD ANGLE AT ACTUATOR ROD CUTOUT HAS ONE CORNER CRACKED. REPAIRED ON FASI WO 20006. N/R 05170- R & R LT INBD MID FLAP LOWER AFT CLOSEOUT CHORD ANGLE AT ACTUATOR ROD CUT OUT AT WBL 108 IAW SRM 57-50-2 FIG. 5 AND 51-40-4 FIGSDR FOTR20006NR5171Skin · dentedLT INBD AFT FLAP INBD LOWER SURFACE HAS 2 LARGE SHALLOW DENTS. REPAIRED ON FASI WO 20006. N/R 05171- REPAIRED LT WING INBD AFT FLAP LOWER SURFACE AT WBL 86.0 BY HOT BONDING REPAIR IAW SRM 51-40-20, REV. 102. MATERIAL USED: DOUBLER; 2024-T3, 0.020", DIM: 11.50SDR FOTR20006NR5184Skin · chafedLT OB FORE FLAP UPPER OB LE WBL 485 HAS A DEEP CHAFED AREA ON THE REPAIR DOUBLER. REPAIRED ON FASI WO 20006. N/R 05184- R & R PREVIOUS DOUBLER AT LT WING OTBD FORE FLAP OTBD L/E AT WBL 485.0 IAW SRM 57-50-4 FIG 1, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.0SDR IPXA10158446Skin · gougedINSPECTION TYPE:4/C, REPAIR SURVEY SEQ. NR 134-W4-01, RT WING INBD FLAP UPPER SKIN REPAIR DOUBLER GOUGED. REPAIRED IAW EO NR A300-5750-36605-A AND EA NR300-5750-01-A2156 IR.SDR IPXA10158421Skin · gougedINSPECTION TYPE:4/C, REPAIR SURVEY SEQ NR 134-W4-02, RT WING CTR FLAP UPPER SKIN REPAIR DOUBLER GOUGED. REPAIRED IAW SRM 57-50-00, PARA. 4E, FIG. 205, PG. 217-220 RE F RCD 385657.SDR IPXA10658388Skin · erodedINSPECTION TYPE:6C, LT WING INBD AFT FLAP INBD FWD (NEAR L/E) FOUND ERODED AND WORN METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR.4 FIG 202 SHEET 1 REV.46.SDR P5CA1001617Flap · delaminatedDURING AIRCRAFT C-CHECK INSPECTION DENT/DELAMINATION WAS FOUND ON THE LT & RT TRAILING EDGE FLAPS AND THE LT INBOARD AILERON. PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 57-53-01 FIGURE 201 REPAIR 1 TABLE 1, SRM 51-70-17 FIGURE 5 AND SRM 57-60-01 FIGURE 201 AS SDR IPXA10158450Skin · chafedINSPECTION TYPE:4/C, LT WING INBD FLAP UPPER SKIN CHAFED. CTR OF FLAP APPROX 18 IN FWD OF RIB STRIP. REPAIRED IAW SRM 57-50-00, FIG. 205.SDR UALA2010012800354Structure · damagedFOUND THREE CRACKS AT INBD MID FLAP LE. 4" LONG, 3.5" LONG AND 2" LONG EA CAUSED BY BIRD STRIKE. SUPPLEMENTAL DATA UPDATE RH IB MIDFLAP OB LEADING EDGE REMOVED RESIN INSTALLED AT BIRDSTRIKE DAMAGE AREA. REMOVED PAINT AND DELAMINATED SKIN. ROUTED OUT CRACKS IN SDR ASAA1047298Skin · dentedRIGHT WING I/B AFT FLAP LEADING EDGE HAS A SHARP DENT 29 INCHES FROM I/B END .5 X .073 A/Y=6.8. SPLICED IN NEW SKIN SECTION .032 2024 T3 IAW B737 400 SRM 57 53 01 FIG 201.SDR SWAA100528Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA100511Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA100508Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR ASAA1047297Skin · dentedDENT RIGHT T/E FLAP 15.5 INCHES FROM I/B EDGE LOWER SURFACE. INSTALLED .016 2024 T6 FILLER & DOUBLER IAW B737 400 SRM 51 70 10.SDR USAA2010012990232Skin · debondedCLT - Q1 - MAJOR REPAIR - LEFT WING OUTBOARD MID FLAP DISBONDED ON LOWER SURFACE 52 INCHES FROM INBOARD END. REPAIRED LEFT WING OUTBOARD MID FLAP IAW B737 SRM 51-70-10.SDR SWAA100537Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA100485Flap · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING O/B FORE FLAP T/E DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA100471Flap · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP I/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER SRM.SDR IPXA10M58502Skin · misrepairedINSP TYPE:4C, REPAIR SURVEY SEQUENCE NR 279-W4-04 RT INBD FLAP LOWER EXISTING REPAIR BTWN STA XIFH 177-183 NOT CORRELATED TO SRM 57-00-01 FIG 7 IS NOT APPLICABLE FOR PRIMARY STRUCTURE ELEMENT. REMOVE DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW STA SSDR IPXA10M58365Vane · delaminatedINSPECTION TYPE:4C, RT INBD FLAP VANE DELAMINATED AT BOTTOM SKIN OTBD END CUT OUT DELAM SKIN 2 IN. DIAM APPLIED WET LAYUP REPAIR REF SRM 57-50-80 REPAIR 2 FIG 201.SDR ASAA1047296Flap · dentedSMALL DENTS ON LOWER SURFACE OF LEFT I/B AFT FLAP. REPAIRED DAMAGED AREAS OF LEFT I/B AFT FLAP IAW B737 400 SRM 51 70 10 REPAIR 4.SDR SWAA100458Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA100455Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR DALA101793212Skin · damagedDURING "L" CHECK FOUND SKIN DAMAGED ON LT OTBD FLAP. REPAIRED IAW SRM 57-53-00.SDR IPXA10658340Hinge Fitting · crackedINSPECTION TYPE:C, RT WING INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE FTG AT IFS179.75. REPAIRED IAW SRM 57-53-02-2R1 FIG201, REV46 BOTH FLANGES CRACK LENGTH AT INBD IS 0.75" & OTBD IS 1" ORG MATL IS 7075T3 FORGING BOTH INSDR IPXA10658339Hinge Fitting · crackedINSPECTION TYPE:C LT WING INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. LT WING INBD MAIN FLAP INBD HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02-2R1 FIG201, REV46 BOTH FLANGES CRACK LENGTH AT INBD IS 1.2" & OTBD IS 0.375" ORG MATL IS 7075T73 FORGING. BOTH SDR UALA2010012600317Skin · gougedLT WING OTBD FLAP UPPER SKIN GOUGED WS 460. UPDATE FLAP SKIN SUSTAINED DAMAGE. REMOVED AND REPAIRED LT WING OTBD FLAP UPPER SKIN PANEL. REINSTALLED FLAP SKIN PANEL.SDR UALA2010012600316Skin · wornRT WING INBD FORE FLAP, UPPER SKIN WORN AT NR8 SPOILER. REPAIRED DAMAGE IAW REO-G13193. THE REPAIR IS A MAJOR REPAIR IAW UA SRM. IT RECEIVED STAGE 1 APPROVAL VIA FAA FORM 8100-9, DATED 20JAN10. A NEW FAA FORM 8100-9 MUST BE ISSUED WITHIN 24 MONTHS FROM 20SDR UALA2010012600315Panel · chafedLT WING INBD FLAP PANEL, OTBD UPPER SURFACE CHAFED. ACP REPAIR IAW REO-G13194. THE REPAIR IS MAJOR REPAIR IAW SRM AND UA EVA 73321, THE REPAIR HAS RECEIVED STG 1 APPROVED VIA FAA FORM 8100-9. CONTINUE, 24 MONTHS FROM 20JAN10 DTA 10-002 HAS BEEN CREATED TO TRSDR IPXA10658260Wedge · damagedOTBD FLAP T/E WEDGE DAMAGED. REPAIR IAW EO B767-5750-35351-C.SDR SWAA100447Rib · crackedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP L/E RIB CRACKED AT WBL 254. REMOVED AND REPLACED RIB PER SRM.SDR SWAA100446Rib · crackedDURING SCHEDULED 22Y CHECK, FOUND LT WING O/B FORE FLAP L/E RIB CRACKED AT WBL 254. REMOVED AND REPLACED RIB PER SRM.SDR ASAA1047271Skin · dentedRIGHT O/B FLAP HAS A DENT ON UNDERSIDE CENTER OF PANEL APPROX I/B END. INSTALLED DOUBLER.
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