JASC 5753
Service difficulty reports · 31,506
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 SWAA2024112656915Bracket · crackedRIGHT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET. STREAMERED<[01] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-8SDR SWAA2024112656917Bracket · crackedLEFT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET OUTBOARD END OF WEB.<[01] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW SDR SWIA202412231104Skin · chafedLH OUTBOARD FLAP INBOARD LOWER LEADING EDGE CHAFFED (C-CHECK RO 12/20/2024) PERFORMED REPAIR ON LH OUTBOARD FLAP PER MHIRJ REO # 670-57-53-388 REV. -- DATED 2024-11-26 AND TASK CARD SKY 51-900-1000 SKY DATE 15 FEB 23. COMPLIED WITH 51-900-1002-SKYSDR IPXA2024112668145Rib · crackedFAULT: THE L/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB 27 AFT SIDE. AREA MARKED IN RED. COMPLIED WITH FINAL UPS E0-92031-REQ1 AND VT MAE EA 300-5750-27-A3726 REV-. AUDIT COMPLETESDR IPXA2024112668047Rib · crackedFAULT: THE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 26 AFT SIDE. AREA MARKED IN RED. COMPLIED WITH FINAL UPS E0-92031-REQ1 AND VT MAE EA 300-5750-27-A3726 REV-. REVIEWEDSDR IPXA2024111667934Rib · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 26 AFT SIDE. AREA MARKED IN RED. VERIFIED EO -92032-REQ1 AND VT MAE EA 300-5750-27-A3729 REV- HAS BEEN ACCOMPLISHED.SDR IPXA2024111667684Rib · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 12 AFT SIDE. AREA MARKED IN RED. VERIFIED E0-92032-REQ1 AND VT MAE EA 300-5750-27-A3729 REV- HAS BEEN ACCOMPLISHED.SDR SWAA2024110856314Skin · delaminatedREPLACE THE LH INBOARD MAIN FLAP DUE TO LOWER SKIN DELAMINATION<[01] REMOVED LH INBOARD MAIN FLAP PER MM 27-51-11;[02] 01 - INSTALLED LH INBOARD TRAILING EDGE FLAP PER [AMM 27-51-11-401-NG (INBOARD TRAILING EDGE FLAP - REMOVAL/INSTALLATION - PERMANENT)];[03] RSDR VNAA20241213008Skin · nickedDISCREPANCY: SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FROM FLS 24.00 TO FLS 65.50 AND WEAR ON AREA OF SETTLEMENT OF FAIRING 583BB AND ACCESS PANEL 584BB SDR VNAA20241213007Skin · nickedDISCREPANCY: SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FROM FLS 24.00 TO FLS 42.00
SDR SWAA2024121256344Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP UPPER AND LOWER SURFACE AT LT WING 2024-687057<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A23325649; DUE DATE: 31-DEC-24;[02] TOOL USED STEP 3: BOND TESTER; P/N: BONDMASTER 600M; S/N: 230106912; DUE DATE: 09 JAN 25.;[SDR IPXA2024110355285Link Assy · brokenFOUND ON FLAP TRACK #5 LINK ASSY BROKEN REPLACED TENSION TIE LINK ASSY IAW AMM 27-51-22-434-016, NO CHANGE OF SHIMS ARE REQUIRED. THIS CLOSES THE DMISDR SWAA2024120655811Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 273 DEFLECTION CONTROL RIB AREA LT WING 2024-633747<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 273 DEFLECTION CONTROL RIB AREA LT WING.IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.TOOL USED .DIGITAL CALIPER P/N:500-19SDR SWAA2024110656113Skin · delaminatedFLT CREW REPORTS LEFT INBD FLAP; AFT OTBD CORNER DELAM<[01] C/W EA 24-157-03032 TSR#2024007736SDR SWAA2024120655754Flap · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE AT LT WING 2024-686013<[01] TOOL USED: CALIPER P/N:500-197-30 S/N: B20189443 DUE DATE: 06-MAR-25.;[02] ON STEP 3; BOND TEST INSTRUMENT P/N: BONDMASTER 600M; S/N: 220052310; DUE DATE: 17-NOV-24.;[03] ON STEPSDR SWAA2024112755393Support Bracket · crackedCRACK INBOARD TRAILING EDGE SUPPORT BRACKET INTERNAL AREA ACCESS PANEL 651DB AT RT WING 2024-672492<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD TRAILING EDGE INTERNAL AREA ACCESS PANEL 651DB AT RT WING IAW B737-700 SRM51-10-02-0G-0; SRM 51-10-02-0G-0 PARAGRASDR AALA202411189769Skin · puncturedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING INBOARD AFT FLAP HAS EVIDENCE OF A PUNCTURE 24 INCHS FROM INBOARD END. ACCOMPLISHED EVALUATION OF EXISTING DENTS AND REPAIRED PUNCTURE ON LEFT HAND INBOARD AFT FLAP LOWER SKIN.SDR AALA202411188799Skin · debondedAIRCRAFT IN BASE MAINTENANCE: DEBONDED OUTBOARD FLAP LOWER SURFACE ON LEFT-HAND WING LOCATED BETWEEN RIB 12 AND RIB 15. PERFORMED PERMANANT REPAIR ON OUTBOARD FLAP LOWER SURFACE PER SRM 57-53-00-300-120.SDR DALA2024110410609Sleeve · wornSHIP 3359 L/H WING O/B FLAP NO.4 REAR LINK FWD ATTACH BOLT AND SLEEVE FOUND WORN. CORRECTIVE ACTION: REMOVED AND REPLACED L/H WING O/B FLAP TRACK NO.4 REAR LINK FWD ATTACH BOLT AND SLEEVE PER A330 AMM 27-54-75. (0639003)SDR SWAA2024112655180Skin Panel · delaminatedDELAMINATED FIXED TRAILING EDGE SKIN PANEL AT LT WING UPPER SURFACE 2024-651169<[01] TOOL USED= CALIPER P/N: 8647A42; S/N: B22058408; DUE DATE: 06-OCT-25;[02] TOOL P/N: FLIR-T530; S/N: 79316000; DUE DATE: 20-FEB-25;[03] TOOL USED HOT BONDER PN: HCS9200B-AV. SNSDR SWAA2024112055350Skin Panel · crackedPERFORM PERMANENT REPAIR ON LH WING TRAILING EDGE UPPER SKIN PANEL 551DT WITH UPPER SKIN CRACK AND EDGE DAMAGE<[01] PERFORMED PERMANENT REPAIR ON LH WING TRAILING EDGE UPPER SKIN PANEL 551DT WITH UPPER SKIN CRACK AND EDGE DAMAGE IAW SRM 51-70-05-2R-6.;[02] VERSDR UIEA2024110101070Seal · missingRIGHT INB AFT FLAP, SEAL MISSING AT O/B SIDE(<P>LOCATED, CLEANED, PREPARED, SECURED, INSTALLED MISSING SEAL AT RIGHT INBD AFT FLAP AREA, BY O/B SIDE, PER BOEING 767 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024110101069Seal · missingLEFT INBD AFT FLAP, SEAL MISSING AT O/B SIDE.(<P>LOCATED, CLEANED, PREPARED, SECURED. INSTALLED MISSING SEAL, AT L/H INB AFT FLAP AREA, BY O/B SIDE, PER BOEING 767 AMM 20-10-23-964-001. NO FURTHER DEFECTS NOTED</P>)SDR DALA2024110110576Drive Assy · gougedSHIP 3160 GOUGE LOWER AREA FLAP DRIVE TRUNNION IB FLAP ON LH WING. CORRECTIVE ACTION: EVALUATED GOUGE LOC ON LOWER AREA FLAP DRIVE TRUNNION I/B FLAP ON O/B FACE LH WING AS PER AIRBUS CMM 57-52-21 SUB TASK 57-52-21. (0638384)SDR SWAA2024121055106Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING. 2024-685138<[01] STEP 3 TOOL USED ULTRASOUND EQUIPMENT PN: GEIT1480179; SN:GOPLS 15100171; DUE DATE: 07-DEC-24;[02] TOOL USED ON STEP 18: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 600. SSDR SWAA2024120654747Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2024-680262<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189443 DUE DATE: 06-MAR-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25-JAN-25.;[03] TOOL USED: ULTRASONIC FLAW DETECTOR P/SDR SWAA2024110554600Fairing · crackedTHE #8 FLAP TRACK FWD FAIRING (644AB) HAS A CRACK ON LOWER SURFACE<[01] REPAIRED CRACK ON #8 FWD FAIRING 644AB IAW SRM 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-7SDR FDEA202410291635Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH I/B FLAP NOSE SKIN BTW RIB 20D~24B COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS SDR SWAA2024110154485Skin · delaminatedLH OUTBOARD AFT FLAP (P/N 113A3700-19; S/N 000992) UPPER SKIN DELAMINATION AT INBOARD EDGE - PERMANENT REPAIR) [TTG8Q00WPEME]<[01] REMOVED AND REPLACED L/H OUTBOARD AFT FLAP PER AMM 21-51-22. CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME. PARTS AND TOOLS ON (TTGSDR UATA7071031245702Flap Track · corrodedRIGHT FLAP MIDDLE FLAP TRACK HAS SEVERE CORROSION INBOARD SIDE. REMOVED AND REPLACED RIGHT FLAP MIDDLE FLAP TRACK IN REFERENCE TO C208 SRM 51-40-00.SDR DALA2024102910489Flap Track · corrodedSHIP 3133 CORROSION ON BORE BEARING TRACK 3 O/B FLAP ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 621101-14. (0633352)SDR SWAA2024102953911Skin · delaminatedLEFT HAND AFT TRAILING EDGE FLAP HAS EVIDENCE OF DELAMINATION TSR # 20244007602<[01] C/W EA 24-157-02971<BR>OKAY FOR CONT SERVICESDR SWAA2024102953726Skin · delaminatedR/H OUTBOARD AFT FLAP LOWER SURFACE IS DELAMINATED AT THE INBOARD END. DELAMINATION MEASURES 8.75' X 7.5'.<[01] REMOVED AND REPLACED R/H O/B AFT FLAP IAW B737 AMM 27-51-22. UP TO ADJUSTMENTS.;[02] REMOVED AND REPLACED R/H O/B AFT FLAP IAW B737 AMM 27-51-22. UPSDR DALA2024102810460Fairing · corrodedSHIP 3133 CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620443-14. (0629881)SDR DALA2024102810459Fairing · corrodedSHIP 3133 CORROSION ON BONDING PLATE FLAP TRACK FAIRING 632CB RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620443-14. (0629879)SDR SWIA202412031024Skin · dentedMUTIPLE DENTS ON LWR SKIN OF R/H WING INBD FLAP. (C-CHECK RO 11/30/2024) MULTIPLE DENTS ON LWR SKIN OF R/H WING I/B FLAP HAVE BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-803, SHEET 1 AND 2. COMPLIED FULLY W/SKYCARD 51-900-1002-SDR IPXA2024120240326Skin · delaminatedLEFT INBOARD FLAP UPPER OUTBOARD SURFACE IS DELAMINATED IN TWO AREAS. DOT AA014. REVIEWEDSDR DALA2024102510415Roller · excess playSHIP 3133 EXCESSIVE PLAY CRUISE ROLLER IB FLAP GUIDE ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER IB FLAP GUIDE ON RH AS PER CMM 57-52-21 TASK 57-52-21-000-805-A0 AND TASK 57-52-21-400-803-A01. (0626045)SDR DALA2024102510414Roller · excess playSHIP 3133 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON LH WING AS PER AIRBUS CMM 57- 53-21, TASK 57-53-21-000-810-A01 AND TASK 57-53-21-400-810-A01. (0626047)SDR SWAA2024112752171Panel · crackedCRACK ON HOLE OF ACCESS PANEL 561BB ON TRAILING EDGE AT LT WING 2024-672178<[01] TOOL USED: CALIPER PN: 500-197-30; SN: B20189443; DUE DATE: 06-MAR-25.;[02] TOOL USED: HOT BONDER PN: HCS9200B; SN: 18165044; DUE DATE: 11-APR-25;[03] TOOL USED: HOT BONDER P/N: HSDR SWAA2024112552374Fitting · corrodedCORROSION FITTING ACCESS PANEL 642BB AT RT WING 2024-645707<[01] REPLACED FITTING AND FASTENERS LOC. ACCESS PANEL 624BB AT RT WING I.A.W. B737-800 SRM 51-40-02 SRM 51-10-02; DWG 113A9350 SHEET 7 REV. E. SEE INDIVIDUAL SING OFFS BELOW.;[02] TASK COMPLETED <BR>SSDR FDEA202410221570Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 170.5 INCHES TO IB AND 7.3 INCHES TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 205 AS PER B777 SRM 57-53-01-2R- 2 AND SRM 51-70-04-2R-1 REV 47.0 AND EA:G-5750-T0381070 P1 TITLE:WING-FLIGHT SURFSDR SWAA2024120251456Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE AT LT WING 2024-671984<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B23316997; DUE DATE: 14-JAN-25.;[02] TOOL USED: ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190984811; CAL DUE DATE: 11-JASDR SWAA2024112551550Angle · crackedCRACK ANGLE LOCATED DEFLECTION CONTROL RIB ORSS279 AT LT WING 2024-645629<[01] REPLACED ANGLE LOCATED DEFLECTION CONTROL RIB ORSS279 AT LT WING IAW B737-800 SRM-51-40-02 AND DWG-115A6200 REV: A;[02] TASK COMPLETEDSDR UIEA2024101801054Skin · dentedINBOARD TRAILING EDGE FLAP RH WING , UPPER SIDE INNER CORNER WITH DENTS(<P> RH WING INBOARD AFT FLAP DENT 1 WAS EVALUATED AND FOUN WITHIN ALLOWABLE LIMITS IAW SRM 57-53-01-1A-1 TABLE I NOTE C DETAIL IV DOT 89020 WAS INSTALLED AS PER ATLAS AIR GMM 3.19.1.</P> /SDR DALA2024102210300Plate · corrodedSHIP 3133 CORROSION FOUND AFFECTING THE IB AND OB AL PLATES AT TRACK #3 LEVEL, IN THE INNER AND OUTER RIB 5. CORRECTIVE ACTION: REPAIR PER ERA 621101-14. (0620476)SDR DALA2024102210299Bearing · corrodedSHIP 3160 CORROSION ON SPHERICAL BEARING O/B FLAP LH WING (2EA) REFER TO AMDS CARD 2750-6020-LT RII. CORRECTIVE ACTION: REPLACED SPHERICAL BEARING FLAP TRACK #3 AND #4 ON O/B FLAP ON LH WING (2EA) AS PER A320 FAM AMM 57-53-21-000-001-A AND 57-53-21-400-001-A. SDR VNAA2024101630024Skin · dentedR/H WING O/B FLAP UPPER SKIN HAS 1EA DENT TOWARDS O/B END.SDR IPXA2024110841640Skin · crackedRH WING INBOARD MAIN FLAP TE WEDGE UPPER PANEL DAMAGE (REPAIR) REPAIRED CRACK ON R/H WING INBD MAIN FLAP T/E WEDGE UPPER PANEL INBD SIDE I.A.W. EGAT EI NO. F2024A57M-2683 REV.0 THROUGH 1 AND UPS EO-91997-REQ1 REV.2.SDR UIEA2024101701047Skin · dentedWING LH, INBOARD FLAP, AFTER FLAP WITH SEVERAL DENTS(<P>ONE DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED.</P>)
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