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 FDEA202404050636Skin · cracked4EA CRACKS (MAX50MM) WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 11 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLER REPAIR AT RIB11~RIB13 S-2.2~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.SDR SWAA2024042571060Skin · delaminatedLT. WING T/E O/B AFT FLAP DELAMINATED ON I/B LWR SKIN.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP PER AMM 27-51-22;[02] 02 - INSPECTED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)]SDR SWAA2024042571039Skin · delaminatedRT. WING T/E O/B AFT FLAP DELAMINATED ON I/B LWR SKIN.<[01] REMOVED RT. WING T/E O/B AFT FLAP PER M/M 27-51-22;[02] OK TO INSTALL NEW SERVICEABLE RT WING OUTBOARD AFT FLAP.;[03] INSTALLED R/H WING T/E O/B AFT FLAP IAW AMM 27-51-22.;[04] C/W CORRECTIVE ACTION#3SDR UIEA2024040500235Skin · corrodedBULGE-SKIN, LOWER FACE OF RH WING T/E FORE FLAP L/E FRONT SPAR LOWER CHORD AREA, WBL 242 AND WBL 244(<P>1. PERFORM PERMANENT REPAIR AT RH WING T/E INBD FORE FLAP LOWER SURFACE WBL 242 ~ WBL 244 IAW EGAT EI T2024A57M-752 REV 1. 2. CONDITION CHECK IS SATISFACTORSDR SWAA2024040570771Fairing · pulled#6 FLAP SUPPORT AFT FAIRING HAS FASTENERS PULLED THRU<[01] 04 - REPAIRED PER [SRM 57-53-70-2R-2-A01234 (REPAIR 2 - FLAP SUPPORT FAIRING - NUMBERS 3 AND 6 INBOARD TRAILING EDGE FLAP - ALTERNATIVE 1 - 500 CYC DVI - INTERIM REPAIR)];[02] VERIFIED WORK PERFORMED ISDR ASAA2024040450033Skin · dentedRIGHT WING, DENT ON I/B FLAP LOWER SKIN, 13 CM FROM UPPER EDGE, .812 MM DEEP, 17MM DIA 220 CM FROM INNER EDGEDOT: B386 GROUNDED - YES. ALL WORK ACCOMPLISHED ON CARD G1941548. PREFORED CATEGORY A PERMANENT REPAIR ON R/W I/B FLAP LOWER SURFACE IN ZONE 2. REPAIRSDR ASAA2024040450032Skin · dentedLEFT WING, I/B FLAP HAS SEVERAL 3 DENTS ON LOWER SKIN ABOVE PYLON FAIRING 7CM LONG 2CM WIDE UNABLE TO MEASURE DEPTH DUE TO FAIRING GROUNDED - YES. REPAIRED LEFT WING I/B FLAP LOWER SKIN LOCATED 13 Ï¿½Ï¿½ FROM OUTBRD AND STOPS AT 10 Ï¿½Ï¿½ AND 8Ï¿½ FROM T/E. ISDR FDEA202404040291Rib · crackedPFM E.A #:6-5750-T0378613 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB 19 BTWN REAR SPAR ~ STRG 2.8 . ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.19 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-57SDR FDEA202404040479Skin · crackedPFM E.A #:6-5750-T0378613 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB19 BTWN REAR SPAR ~ STRG2.8. ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.19 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-SDR DALA2024040504107Housing · corrodedSHIP 3139 CORROSION FOUND IN TRACK 2 SUPPORT BEARING HOUSING AT RIB 9 LEVEL. CORRECTIVE ACTION: REPAIRED PER ER/A 616560-14. (0277901)SDR 21GA20240404010Flap Track · wornOUTBOARD FLAP TRACK SUPPORT BEAMS NO.'S 1, 2, 7, AND 8 ATTACHMENT HOLES BUSHING REPAIR.SDR UIEA2024040500241Skin · dentedDENT- PANEL 587LT EXTERNAL, LH OUTBD MID FLAP WBL 582(<P>1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD MID FLAP TOP PANEL 587LT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISDR UIEA2024040500240Skin · dentedDENT- LH OUTBD FORE FLAP OUTBD TOP PNL EXTERNAL WBL 655(<P>1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD FORE FLAP TOP PANEL EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISFASDR UIEA2024040500239Skin · dentedDENT PANEL 677IT EXTERNAL SURFACE, RH INBD MID FLAP WBL 373.33(<P>1. PERFORM REPAIR OF DENT SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SDR UIEA2024040500238Skin · dentedDENT- SKIN, R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACEWBL 374.83(<P>1. PERFORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDISDR YENA2024040500495Skin · damagedFLT#1359, JFK-KIN. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK AND DECLARED AN EMERGENCY) 'DEPARTING JFK POSSIBLE LIGHTNING STRIKE RIGHT LOWER OF NOSE, NO SYSTEMS ABNORMAL; FOUND DAMAGE ON #4 L/H FLAP FAIRING 533DB PLACED ITEM ON CDL REF LP 3959263, ITEM 2 (APSDR 21GA20240403006Fitting · damagedRH WING INBOARD FLAP-OUTBOARD LINKAGE FITTING BLEND OUT REPAIR.SDR AALA202405291984Trunnion · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP TRUNNION WORN AT RIB 1 AND WXO. REPLACED FLAP TRUNNION PER TASK CARD 26L00027003.SDR IPXA2024042701079Skin · dented**SDR FILED OPEN**FAULT - LH OUTBOARD FLAP HAS DENT IN LEADING EDGE VERIFIED TOP COAT APPLICATION STEP 49.SDR DALA2024040203987Fairing · damagedSHIP 3142 #4 FLAP TRACK FAIRING ON LEFT WING DAMAGED BY DEPARTURE OF PANEL 575GB. CORRECTIVE ACTION: REPAIRED PER A319 SRM 57-51-37-400-004-A. (5402308)SDR DALA2024040103928Bearing · corrodedSHIP 3139 CORROSION ON SPHERICAL BEARING FLAP TRACK 4 OF THE FLAP OUTBOARD. CORRECTIVE ACTION: REPLACED SPHERICAL BEARING TRACK 4 ON O/B FLAP LH WING AS PER A320 FAM AMM 57-53-21-000-001-A AND AS PER A320 FAM AMM 57-53-21-400-001-A. (0271631)SDR SWAA2024051068886Skin · debondedDEBONDED OB AFT FLAP LOWER SURFACE IB SIDE AT LT WING. PERFORMED INTERIM REPAIR ON O/B AFT FLAP AT LT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16 AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYC OR 30 MONTHS.SDR UIEA2024032100166Skin · torn#8 V/C FLAP LSA FOUDN TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2024032100170Skin · torn#9 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA AS PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.SDR UIEA2024032100172Skin · torn#6 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2024032100178Skin · torn#7 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2024032100180Skin · torn#21 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2024032100181Skin · torn#20 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2024032100182Skin · torn#19 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2024032100183Skin · torn#18 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER SMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2024032200189Repair · torn#10 V/C FLAP EXISTING PATCH FOUND TORN. PERFORMED REPAIR AT EXISTING PATCH TORN AREA PER SRM 51-70-04 REPAIR 7. NO FURTHER DEFECTS NOTED.SDR DALA2024040103935Hinge · obstructedINTERFERENCE BTW HEAD BOLT AND FWD OUTB FLAP HINGE AT RH WING. SUMMARY OF NRC 00808: FWD OUTB FLAP HINGE AT RH WING WAS REPAIRED PER ERA 616905-14 REV ORIGINAL SECTION I. ASSOCIATED ER/A 14-616905 ADDED FOR AC 9522. (LP #0268113)SDR FDEA202403290404Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. MAJOR REPAIR SDR FDEA202403290403Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE 1EA CRACK AT RIB21 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLSDR FDEA202403290402Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB25, RIB26, RIB27 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE 5EA CRACKS AT RIB25, RIB26, RIB27 BETWEEN STGR2.SDR FDEA202403290401Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB26, RIB27 BETWEEN STGR2.6 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378625 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE 3EA CRACKS AT RIB26, RIB27 BETWEEN STGR2.6 AND REAR SPARSDR FDEA202403290400Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378625 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE 1EA CRACK AT RIB17 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING -SDR DALA2024040103933Cover · missingAIRCRAFT 3004, FOUND LH #4 FIXED FLAP TRACK BOTTOM COVER MISSING. CORRECTIVE ACTION: REPLACED COVER IAW A321 AIPC 57-55-05-24D ITEM 20. OK FOR SERVICE AT THIS TIME. (LP 5523679)SDR LR7A2024032803388Skin · dentedDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5712, FOUND RH OB FLAP UPPER TRAILING EDGE SKIN DENTED AT OWFS41R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001086441. / PSE# 57-50-16, AD 2012-06-09SDR LR7A2024032803386Skin · crackedDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5712, FOUND RH OB FLAP UPPER SURFACE BAFFLE ASSEMBLY CRACKED AT OWFS2R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001086406 / PSE# 57-50-16, AD 2012-06-09SDR SWAA2024032868544Skin · delaminatedDURING WALK AROUND; FOUND DELAM AT R/H I/B AFT FLAP ON A PRIOR REPAIR DELAM ON EXISTING REPAIR AT R/H I/B AFT FLAP. 13 FROM I/B EDGE 3 FROM TRAILING EDGE. DELAM AREA 6 BY 6. SEE ATTACHED PIC FOR DETAILS.<[01] CW EA 24-157-00828SDR VNAA20240425020Bushing · corrodedCORROSION ON BORES OF LUGS (2EAS) AT HINGE NO.4 WAS FOUND AT LH WING TRAILING EDGE. BORES OF LUGS (2EAS) AT HINGE NO.4 WAS FOUND AT LH WING TRAILING EDGE WERE REPAIRED PER PER REO 690-57-51-345 REV. - -SDR CALA2024032900904Skin · peelingPDA 1 RIGHT OUTBOARD TRAILING EDGE FLAP HAD A PIECE OF SKIN PEEL OFF APPROX 288 SQUARE INCHES ON THE INBOARD SIDE OF THE RIGHT OUTBOARD TRAILING EDGE FLAP ,AS PER GMM 02-30-95 THIS WOULD BE CONSIDERED CATEGORY 1 ITEM ITEM SHOULD GENERATE FRM CODE UAL53991. TOSDR UIEA2024032300206Skin · dentedRIGHT WING INBOARD AFT FLAP UPPER SKIN WITH TWO DENTS(<P>UPPER SKIN WAS REPAIRED SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)SDR KCSA202403271036Fitting · crackedO/B GUIDE ROLLER FITTING CRACKED ON L/H I/B FLAP.SDR DALA2024032703843Strut · corrodedSHIP 3139 CORROSION IB FLAP INTERCONNECTING STRUT INTERNAL AREA AND MISSING LABE L TOP ON RH WING. CORRECTIVE ACTION: REPLACED IB FLAP INTERCONNECTING STRUT ON RH WING AS PER A320 FAM AMM 27-51-44-000-001-A AND AS PER A320 FAM AMM27-51-44-400- 001-A. (0264143)SDR VNAA20240426007Skin · nickedINITIAL INSPECTION: SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01, EVALUATED, BTW INBOARD FSDR SWAA2024042567680Plate · crackedCRACK CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS242 AT LT WING. REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED ORSS242 AT LT WING; IAW BOEING 737-700 SRM 51-40-02 AND BOEING 737-700 SRM 51-10-02 ITEM 9.SDR IXXA2024041001Skin · delaminatedRIGHT WING, OUTBOARD FLAP, UPPER SURFACE, 36 INCHES+- FROM INBOARD EDGE AND 28 INCHES FROM TRAILING EDGE IS AN AREA OF DELAMINATIONSDR CALA2024032700882Seal · missingLEFT WING INBOARD FLAP AERODYNAMIC RUBBER SEAL DEPARTED AIRCRAFT. SEAL MEASURES 39.4 INCHES IN LENGHT. INSPECTED AND FOUND SEAL TO BE MISSING FROM A/C. INSTALLED NEW AERODYNAMIC SEAL ON LEFT WING FLAP INBOARD TRACK REF AMM 27-51-00.
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