JASC 5753
Service difficulty reports · 31,513
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 FDEA202110312692Bracket · corrodedLEFT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE CORROSION. CORROSION AT LEFT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-SDR FDEA202110312691Bracket · corrodedLEFT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE CORROSION. CORROSION AT LEFT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11SDR FDEA202110312690Fitting · damagedRIGHT HAND WING-OUTBOARD FLAP VANE ASSEMBLY. FITTING (F) ECCENTRIC HOLE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (F) ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5. FIGURE 201. OVSDR FDEA202110302679Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHISDR FDEA202110302678Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHINSDR DALA2021110106708None · noneSHIP 3256 ELONGATED HOLE FUEL TANK LOWER SURFACE CUT OUT OF ACCESS PANEL BTW RIB 16 TO RIB 17 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 57-21-11. (2001332)SDR SWIA20250514029Skin · dentedDENT ON LOWER SKIN OF INBOARD LH FLAP FOUND TO BE OUT OF LIMITS (FILED CLOSED)REPAIRED DENT ON LOWER SKIN OF INBOARD LH FLAP IAW CRJ 700 SRM 57-52-01SDR FDEA202110292656Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE FOUND CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSDR FDEA202110292655Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZESDR FDEA202110292657Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED SDR FDEA202110292654Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP AFT HINGE BRACKET PIVOT INBOARD LUG BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED SDR FDEA202110272631Bracket · corrodedLEFT HAND WING- INBOARD FLAP ASSEMBLY. OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE CORROSION. CORROSION AT LEFT HAND WING-INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE REWORKED AND FOUND WITHIN LIMITSDR SWAA2021111733974Rib · crackedR/H WING T/E OTBD OF SAIL TAIL; ATTACH CLIP AT INBD SIDE OF DEFLECTOR RIB CRACKED. / REMOVED DAMAGED ATTACHMENT CLIP IAW B737 SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW CLIP IAW BOEING DWG 115A6200 REV B. INSTALLED NEW CLIP ON R/H WING SAIL TAIL DEFLECTOR IAW BSDR LR7A2021091102982Skin · crackedSUPPLEMENTAL INFORMATION DURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND R/H OUTBOARD FLAP UPPER SKIN CRACKED AT OWFS81R, 8 INCHES FROM TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000577135.SDR 7C7A2021102300030None · noneRH FLAP LOWER SKIN DAMAGEAT STA YW316.00. REPAIRED IAW RD8-57-9302SDR FDEA202110222591Hinge Bracket · corrodedRIGHT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE CORROSION. CORROSION AT RIGHT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-SDR FDEA202110222593Bracket · corrodedRIGHT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE CORROSION. CORROSION AT RIGHT HAND WING- INBOARD FLAP ASSEMBLY . OUTBOARD AFT HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MSDR DALA2021102206564None · noneSHIP 3260 L/H I/B FLAP AFT LOWER SKIN HAS DENT AND PUNCTURE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-52-00, AND RESTORED FINISH PER A320 SRM 51-75-12. (1991136)SDR SWAA2021112331106None · debondedCUSTOMER REQUEST DEBONDED IB MAIN FLAP WEDGE PANEL AT RT WING ; 2021-486468 / [01] REPLACED IB MAIN FLAP WEDGE PANEL AT RT WING. IAW B737-700 SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.; [02] CERTIFIED WORK PERFORMED.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.SDR SWAA2021111831914None · delaminatedL/H OUTBOARD AFT FLAP DELAMINATED INBOARD CORNER. / REMOVED AND REPLACED L/H O/B AFT FLAP PER AMM 27-51-22- SA-M# A1184777- (D62)POS- L/H TAG # 14938-P/N OFF- 113A3700-19 S/N OFF 001476 P/N ON- 113A3700-25 S/N ON- 003991.SDR AALA202111021749Flap · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATION IN LOWER SKIN OF LH OUTBD FLAP AT WSTA 810.50, 11.0 IN FWD OF TRAILING EDGE, MEASURING L=2.0 IN, W=2.0 IN. ACCOMPLISHED PERMANENT REINFORCING BONDED REPAIR IAW SRM 57-53-01-2R-2 AND 51-70-04-2R.SDR AALA202111014977Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATION OF OUTBD FLAP LOWER SKIN OF LH WING AT WSTA 810.50, 11.0 IN FWD OF TRAILING EDGE, MEASURING L=2.0 IN, W=2.0 IN. ACCOMPLISHED PERMANENT REINFORCING BONDED REPAIR IAW SRM 57-53-01-2R-2 AND 51-70-04-2R.SDR DALA2021101806377Strut · corrodedSHIP 3119 - L/H FLAP I/B SIDE INTERCONNECTING STRUT HOUSING CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED L/H FLAP INTERCONNECTING STRUT. IAW A319 AMM 27-51-44. (1984487)SDR DALA2021101806376Strut · corrodedSHIP 3119 - R/H FLAP I/B SIDE ON INTERCONNECTING STRUT HOUSING CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED R/H FLAP INTERCONNECTING STRUT. IAW A319 AMM 27-51-44. (1984477)SDR FDEA202110142563Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.SDR FDEA202110142562Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27FWD AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.SDR FDEA202110142561Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 26AFT AREA(REAR) OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGSDR FDEA202110142559Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP 27AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO:6-5750-T0364642, TITLE:WING-FLIGHT SURFACES- LHCENTER FLAP, CRACK IN UPPER FLANGE OF RIB27 AT STRINGERS2.8 -ALI575306-01 & A300- 600SDR DALA2021111807128Vane · unknownCRACKED, PHENOLIC RUB STRIP ON TOP SKIN. LOOSE/MISSING HARDWARE, OUTBD ROLLER FITTING. DENTS, UPPER AND LOWER SKIN. BUMPERS WORN. ONE DENT ON LEADING EDGE FOUND TO BE OUT OF LIMITS PER B717 SRM 57-53-01-01A. MAINTENANCE REPAIRED THE UNIT AS SPECIFIED IN BLOCK(SDR DALA2021101306315None · noneSHIP 678 WORN ON L/E (BTW MFSTA 300 TO 309) AT RH WING OUTBRD MAIN FLAP. CORRECTIVE ACTION: SUMMARY OF NRC 00325 : L/E (BTW MFSTA 300 TO 309) AT RH WING OUTBRD MAIN FLAP. WAS REPAIRED PER ETI-57-21-504 REV. 5 AND ERA 594582-14 REV ORIG. SECTION I PERMANENT REPSDR SWIA202163526None · chafedR/H I/B FLAP LEADING EDGE PANEL 684LB IS CHAFED (C-CHECK RO 1/7/2022) ORDERED AND RECIEVED NEW PANEL# 684LB. SEE CONTINUATION CARD FOR WORK PERFORMED AND SEE JOB# 71029870 OP# 7006 TRANS# 23487017 FOR INSTALL OF PANEL# 684LB.SDR SWAA2021111829276Panel · crackedFLAP SUPPORT NO.8 PANEL 644EB LOWER SECTION CRACKED/DELAMINATED ; / [01] REMOVED DAMAGED PLIES AND PREPARED DAMAGED AREA FOR REPAIR AT PANEL 644EB AS PER B737-700 SRM 51-70-04-2R-0; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR; [03] REPAIRED DAMAGED AREA AT PANESDR IPXA2021100974769Flap · noneINSPECTION TYPE:A300RT WING O/B FLAP O/B STATIC WICK BASE DIBONDED. AFTER FURTHER INVESTIGATION FOUND FLAP SKIN WITH CORROSION. MATERIAL REMOVED DOWN TO 0.043' (78%) WITH SOME CORROSION STILL REMAINING.ACCOMPLISHED DOUBLER SKIN REPAIRED PER EA #300-5754-27-A27SDR SWAA2021111527492Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP EXTERNAL SKIN LOWER SURFACE LOCATED AT INBOARD CORNER ON LT WING ; 2021-466030 / [01] EVALUATED DAMAGED ON OUTBOARD AFT FLAP EXTERNAL SKIN LOWER SURFACE LOCATED AT INBOARD CORNER ON LT WING AND FOUND WITHIN LIMITS TO REPSDR DALA2023051203744Unknown · unknownSOME DENTS ON RIGHT FLAP MOVEABLE AFT VANE RH WING (AD). ADDL TIME RLTD MON 1972923 ADDED. SUMMARY OF NRC 00161: 57 DENTS ON RIGHT FLAP MOVEABLE AFT VANE RH WING WERE MEASURED WITH A LARGER DIMENSION: DEPTH: 0.015 IN, DIAMETER: 0.599 IN, DIAMETER/DEPTH: 0.599 SDR SWAA2021100424275Bulkhead · crackedRIGHT WING I/B FIXED TE UPPER BULKHEAD ASSY CRACKED ; / [01] R&R RIGHT WING I/B FIXED TE UPPER BULKHEAD ASSY AS PER AMM 20-50-11.SDR SWAA2021102723715Panel · pulledRT WING T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES. FABRICATED REPAIR PLIES AND INSTALLED, LEAK CHECKED GOOD IAW SRM 51-70-04-2R-9.PARA 4.J-M.SDR DALA2021092905879Flap Track · out of alignmentF/CTL FLAPS LOCKED AND F/CTL FLAP SYS 2 FAULT. T/S PER A321 TSM 27-51-00-810-818-A. FOUND LH FLAP TRACK NO.1OUT OF ALIGNMENT. PERFORMED FLAP TRACK ADJUSTMENT PER A321 AMM 27- 54. PERFORMED OPS TEST OF THE FLAP SYSTEM . OPS CHECK OK. (EP 626468) RII COMPLETED QSDR FDEA202109242488Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB 26AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364452 P1, TITLE: WING-FLIGHT SURFACES-LH CENTER FLAP, CRACK IN UPPER FLANGE OF RIB26 AT STRINGERS 2.8-ALI 575306-0SDR SWAA2021092722201None · delaminatedSUPPLEMENTAL INFORMATION: LEFT WING O\B AFT FLAP I\B LOWER CORNER DELAMINATED APPROX 6'X7'. ; / [01] R&R LH AFT FLAP REF 27-51-22SDR FDEA202109232362Fitting · crackedRIGHT HAND WING - INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT AFTER REMOVAL FOUND LOWER FORWARD ANGLE CRACKED AT LOWER FORWARD INBOARD AREA . RIGHT HAND WING INBOARD TRAILING EDGE FLAP INBOARD LOWER SEGMENT LOWER FORWARD STATION TR XIFH 133.90 CRACKEDSDR FDEA202109232395Panel · damagedLEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPMISDRILLED HOLE AT I/B CORNER OF OUTBOARD END. REPAIRED PANEL PER E.A. 8-5710-T0364140(P1)- BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501 (MAJOR REPAIR)SDR FDEA202109232394Panel · damagedLEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPS HAS MISDRILLED HOLES. REPAIRED PANEL PER E.A. 8-5710-T0364140 (P1)-BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501(MAJOR REPAIR)SDR FDEA202109222354Hinge Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY, INBOARD FORWARD HINGE (WING SIDE) BARREL NUT SURFACE CORROSIONSDR FDEA202109202350Wedge · wornRH WING, SLAT NO 8 WITH GOUGE ON TRAILING EDGE WEDGE L=30MM, W=18MM, D=1MM. RH WING SLAT #8 TRAILING EDGE WEDGE, LOWER SKIN WAS REPAIRED I.A.W. SRM 57-43-02-2R FIG. 201 (SHEET 1) PAG. 1-2 AND SRM 51-70-10-2R FIG. 202 (SHEET 8) PAG. 15-23,53,71-79,84,162 RSDR FDEA202109202349Skin · chafedRIGHT WING, OUTBD MAIN FLAP, CENTER LEADING EDGE SKIN HAS 2EA WEAR SPOTS. REPAIRED RH WING OB MAIN FLAP IAW EA F-5750-T0364593-P1,SDR IPXA2021091974035Skin · damagedDAMAGE TO THE UPPER SKIN OF THE FLAP REQUIRES REPAIR. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO A300-5750-81573-BSDR FDEA202109182348Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY,FITTING (D) ECCENTRIC HOLE CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (D) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FSDR FDEA202109182347Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY,FITTING (F) ECCENTRIC HOLE CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (F) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FSDR FDEA202109182346Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY,FITTING (C) ECCENTRIC HOLE CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (C) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R. REPAIR 5
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