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 FDEA202112243133Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR FDEA202112243132Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- SDR FDEA202112243131Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-SDR DALA2021122708048None · noneSHIP 3263 CORROSION INTERCONNECTING STRUT OB FLAP ON CONNECTOR LH WING. CORRECTIVE ACTION: REMOVED AND REPLACED CONNECTOR ON INTERCONNECTING STRUT LH WING AS PER A320 AWM 27-51-12. (2063606)SDR AALA202201071752Tab · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP TAB UPPER SURFACE SKIN DELAMINATED 11.5 INCHES FROM THE INBOARD EDGE. REPAIRED FLAP TAB PER SRM 57-52-00-300-088.SDR FDEA202112173100Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PSDR FDEA202112173099Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PERSDR FDEA202112173098Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PERSDR FDEA202112173097Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACH INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MSDR GTIA2023071337324Flap · dentedREF LP 285046901 RH OB FLAP DENT-REPAIRED IAW EO 5753-2129. MOC NOTIFIED.SDR SWAA2022020753923Doubler · debondedR/WING OUTBOARD AFT FLAP I/B LOWER CORNER DISBONDED ; / [01] REMOVED THE ALUMINUM SKIN DAMAGED (CUT OUT 1'' DIAMETER) AND PREPARED AREA TO APPLY DRY OUT. REF B737-700 SRM 57-53-01-2R-14; SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0 PARAGRAPH 7.; [02] VERIFIED STEP SDR SWAA2021122053710Rod · brokenRIGHT I/B TE FLAP HANGING DOWN WITH FLAPS UP. REPLACED BROKEN AFT FLAP DRIVE ROD AND DRIVE ROD FITTING IAW AMM 27-51-14. OPS CHECK GOOD.; [02] VERIFIED CORRECT INSTALLATION OF FLAP DRIVE ROD PER AMM 27-51-14.SDR SWIA202163361None · damagedFLAP TRACK CARRIAGE FOR 632BB HAS DAMAGED PHENOLIC ON OB LUG. (C-CHECK RO 12/29/2021) REMOVED AND REPLACED BUSHING ON FLAP TRACK CARRIAGE FOR 632BB OB LUG . AMM 20-10-08SDR SWIA202163360None · damagedFLAP TRACK CARRIAGE FOR 623BB HAS DAMAGED PHENOLIC ON OB LUG. (C-CHECK RO 12/29/2021) REMOVED AND REPLACED OB LUG BUSHING ON FLAP TRACK CARRIAGE FOR 623BB. AMM 20-10-08SDR SWAA2022012052997Fairing · crackedCRACK FLAP TRACK FAIRING 644BB FORWARD POSITION AT RT WING ; 2021-558252 / [01] TOOL USED: CALIPER P/N 500-464 S/N 15331926 DUE DATE 28-SEP-22.; [02] SCALE P/N: SCA-301 S/N:AE-412125 DUE DATE 24 FEB 22.; [03] HOTBONDER P/N:HCS9200B S/N:13061394 DUE DATE: 05 AUSDR SWAA2021122052809Skin · delaminatedRIGHT WING-OTBD TRAILING EDGE -AFT FLAP-DELAMINATED AT INBD END. REMOVED AND REPLACED R/H OUTBOARD AFT FLAP PER MM 27-51-12SDR AALA202202098516Pendulum · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE FLAP TRACK #4 PENDULUM ASSEMBLY. REPLACED PENDULUM ASSEMBLY PER CMM 57-53-21-400-809-C01 AND SRM A319 57-72-11-911-001.SDR LR7A2021121303066Skin · crackedDURING SCHEDULED C-9 CHECK UNDER JOB CARD HC2711, FOUND LH OUTBOARD FLAP UPPER SKIN CRACKED THOUGH RIVET HOLE AT OWFS153-157L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0843. / PSE# 57-50-16, AD 2012-06-09SDR LR7A2021121303065Skin · crackedDURING SCHEDULED C-9 CHECK UNDER JOB CARD HC2711, FOUND RH OUTBOARD FLAP UPPER SKIN CRACKED THOUGHT RIVET HOLES AT OWFS187-193R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0840. / PSE# 57-50-16, AD 2012-06-09SDR LR7A2021121303064Skin · dentedDURING SCHEDULED C-9 CHECK UNDER JOB CARD HC2711, FOUND RH OUTBOARD FLAP LEADING EDGE UPPER SKIN DENTED AT OWFS259R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0839. / PSE#57-50-16, AD 2012-06-09SDR SWAA2022011852349Rib · crackedL/W I/B FLAP L/E SECOND RIB IS CRACKED.(FROM I/B). ; / [01] REMOVED DAMAGED RIB AT L/W I/B FLAP L/E AREA UNDER PANEL #553AT; AS PER B737-7; SRM 51-40-02-0G-0.; [02] FPI ACCOMPLISHED AT IN-PROGRESS FABRICATION OF RIB AFTER ALL MACHINING IAW BOEING DRAWING # PL1SDR SWAA2022010451815Skin · delaminatedL/H WING O/B AFT FLAP AREA OF DELAM ON UPPER SURFACE 78.5' O/B OF I/B EDGE AND 2' FWD OF AFT EDGE ; / [01] BOND TEST IAW B737 NDT PART 4; 51-00-05. DISBOND AREA MARKED IN BLACK. TOOL#40082; DUE 11OCT22; [02] EVALUATED AND FOUND DELAM 1/2 INCH DIAMETER AND REPASDR FDEA202112093072Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUNSDR FDEA202112093071Hinge 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 EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHSDR FDEA202112093070Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND SDR FDEA202112093069Hinge 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 EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHINSDR FDEA202112093068Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. REPSDR FDEA202112093067Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE SURFACE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. REPAIRSDR FDEA202112093066Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR FDEA202112093065Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-SDR FDEA202112093064Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. SDR FDEA202112093063Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 5SDR FDEA202112093062Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR DALA2021121707844None · noneSHIP 3257 CORROSION INTERCONNECTING STRUT IB FLAP ELECTRICAL CONNECTOR 7541VC AND 7543VC ON LH WING. CORRECTIVE ACTION: REPLACED PER A320 AMM 27-51-11. (2046531)SDR SWAA2022010450942Support Fitting · cracked#6 FLAP SUPPORT FITTING CRACKED. DOT#A193-1 ; / [01] REMOVED #6 I/B FLAP TRANSMISSION ATTACH FITTING IAW AMM 27-51-31-000-801 STEP 2.E.(5).(B) & AMM 27-51-15-000-801 STEP 2.F.(5).; [02] LINED REAMED #6 FLAP TRANSMISSION INBOARD SUPPORT FITTING IAW BOEING CMM 5SDR HALA2021120900221Lug · corrodedSHIP 385 Z570 LH MLG RIB 6 FWD & AFT LUGS MODIFICATION AS PER 5753-01163-08A. CORROSION REMOVAL AT FWD LUG BORE & AFT SPOTFACE FOUND BEYOND LIMIT PER FIG 01, SHT 2. CORROSION REMOVAL AT AFT LUG AFT SPOTFACE FOUND BEYOND FIG 01, SHT 2. CORRECTIVE ACTION: CARRIESDR HALA2021120700220Lug · corrodedSHIP 385 Z670 LH MLG: WHILE PERFORMING EM 5753-01164 A330 SB 57-3124 R3, CORROSION WAS FOUND ON THE LH RIB 6 FWD LUG BORE AND AFT FACE AND THE AFT LUG AFT FACE. CORRECTIVE ACTION: BUSHES REWORKED AS PER ER/A 594564-14AD. (2043724)SDR HALA2021120700219Rib · corrodedSHIP 385 Z670 RH MLG: RIB 6 FWD & AFT LUGS MODIFICATION AS PER 5753-01163 -08B. CORROSION REMOVAL AT FWD LUG FWD & AFT SPOTFACE FOUND BEYOND LIMIT. CORRECTIVE ACTION: CARRIED OUT AIRBUS REPAIR INSTRUCTION R575-58741 ISSUE E. ASSOCIATED ER/A 14-594565. (2043711SDR HALA2021120700218Rib · corrodedSHIP 385 WHILE PERFORMING EM 5753-01164 (A330 SB 57-3124 R3), CORROSION WAS FOUND ON THE RH RIB 6 FWD LUG BORE AND FWD AND AFT FACES. CORRECTIVE ACTION: RBUSHES REWORKED AS PER ER/A 594565-14AD. (2043706)SDR FDEA202112073041Skin · noneLEFT WING INBOARD MAIN FLAP UPPER SURFACE HAS 1 DENT REPAIRED LEFT WING INBOARD MAIN FLAP UPPER SURFACE SKIN IAW B757 SRM 57-53-01-2R AND B757 SRM 51-70-10-2RSDR HALA2021121000224Fitting · corrodedSHIP 385 CORROSION WAS FOUND ON THE RH RIB 6 FITTING. CORRECITVA ACTION: REF ERA 594565-14. (2043088)SDR HALA2021121000223Fitting · corrodedSHIP 385 CORROSION WAS FOUND ON THE L/H RIB 6 FITTING. CORRECTIVE ACTION: REF ERA 594564-14AD. (2043034)SDR SWAA2022012450378Retainer · crackedRIGHT WING T/E VERTICAL BULB SEAL RETAINER LOCATED ABOVE AFT PYLON FAIRING AFT TIP AT ORSS 278 IS CRACKED ; / [01] REPLACED R/W T/E VERTICAL BULB SEAL RETAINER ABOVE AFT PYLON FAIRING AFT TIP AT ORSS 278 IAW SRM 51-40-02-0G-0; [02] VERIFIED ACTION 1SDR AALA202112229214Tab · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING OUT BOARD TRAILING EDGE FLAP TAB DELAMINATED AT HINGE 3B AND TAB RIB 3. REPAIRED FLAP TAB PER SRM 57-53-00-300-094.SDR SWAA2021121450502Fairing · cracked#3 FLAP TRACK FAIRING 542BB FORWARD OUTBOARD EDGE CRACKED. ; / [01] EVALUATED AND FOUND FWD O/B EDGE CRACKED AS MARKED. TAP TEST GOOD AROUND DAMAGE. FOUND TO BE REPAIRABLE IAW SRM 57-53-70-2R-4 REPAIR 4 TABLE 201 AND SRM 51-70-04-2R-10.<BR><BR>CLEANED AND PREPSDR SWAA2021120850426Skin · delaminatedL/H O/B AFT FLAP HAS DELAM I/B LOWER SURFACE ; / [01] REMOVED AND REPLACED LH OB AFT FLAP REF AMM 27-51-22.SDR AALA202112062687Flap · delaminatedAIRCRAFT WAS GROUNDED: TOP SIDE OF LEFT OUT BOARD AFT TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED LEFT OUT BOARD AFT FLAP PER AMM 27-51-21.SDR AALA202201312679Flap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUT BOARD FLAP OUTER DOUBLER BETWEEN RIB 14 AND RIB 15 AND S7 AND S10. REPLACED FLAP TASK CARD 26L00027009.SDR AALA202112218358Flap · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE DELAMINATED BETWEEN RIB 6 AND RIB 8. REPAIRED FLAP PER SRM 57-52-00-300-094.SDR SWAA2021121348814Fairing · delaminated#8 FLAP AFT CANOE FAIRING IS DELAMINATED ON LOWER AFT END. ; / [01] REMOVED AND REPLACED #8 AFT CANOE FAIRING PER REF SRM 51-40-02; [02] INSPECTED WORK PERFORMED
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