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 SWAA2024060685971Skin · delaminatedLEFT WING OUTBOARD FLAP AFT FLAP INBOARD UPPER SURFACE HAS DELAMINATED AREA AS MARKED<[01] 04 - REPAIRED PER [SRM 57-53-01-2R-14-B00296 (REPAIR 14 - OUTBOARD AFT FLAP TRAILING EDGE WEDGE - PERMANENT)];[02] AUDIT C/WSDR SWAA2024060685978Skin · delaminatedRIGHT WING OUTBOARD FLAP AFT FLAP INBOARD UPPER SURFACE HAS DELAMINATED AREA AS MARKED<[01] REPAIRED DAMAGE TO R/H WING OUTBOARD AFT FLAP IAW SRM 57-53-01-2R-14 AND SRM 51-70-10-2R-0 REPAIR GENERAL;[02] AUDIT C/WSDR SWAA2024053085707Skin · delaminatedL/H O/B AFT FLAP HAS DELAMINATION AT I/B LOWER CORNER LOWER SURFACE.<[01] REMOVED L/H O/B AFT FLAP ASSY. REF AMM 27-51-22;[02] INSTALLED L/H O/B AFT FLAP. REF AMM 27-51-22. PENDING ADJUSMENT CK.;[03] 02 - INSPECTED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP -SDR VNAA20240524004Skin · crackedSEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 42 AT RH WING WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01 AND LOWER SKIN OF LH INBOARD FLAP FLS 42 TO FLS 65.5 WAS EVALUATSDR DALA2024051505223Vane · dentedDENTS ON AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING. SUMMARY OF NRC 00238: AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING WAS REPAIRED PER ER/A 617597-14 REV ORIGINAL. ASSOCIATED ER/A 14-617597 ADDED FOR AC 9538. (LP #0342649)SDR DALA2024051505222Skin · crackedDENT WITH CRACK (1 EA) 19" FROM OTBD EDGE AND 5.500" FROM LEADING EDGE AND DENT WITH DISBOND (1 EA) 34" FROM OUTBD EDGE AND 4" FROM TRALING EDGE ON LOWER SURFACE AT AFT FLAP MOVABLE VANE AT RIGHT WING. SUMMARY OF NRC 00563: LOWER SURFACE AT AFT FLAP MOVABLE VASDR SWIA20240813513Hinge · corrodedLH INBD FLAP THE INBD HINGE BOX HAS SIGNS OF CORROSION AT HINGE POINT (MARKED) (C-CHECK RO 8/11/2024) PERFORMED REPAIR OF L/H I/B FLAP HINGE BOX CORROSION AT HINGE POINT BY COMPLYING WITH ALL STEPS OF REO 670-57-54-062 REV -- DATE 2024-06-24 COMPLIED WISDR ASAA2024051351516Skin · delaminatedLESSOR ITEM: D&B #2 NON ROUTINE 00204 RECORDS A CONCENTRATION OF DENTS, THE CLOSING DOCUMENTS NEITHER RECORD HOW MANY NOR DIMENSIONS AND LOCATIONS. PLEASE RE-ASSES AND ADD SRM REFERENCE USED AND PICTURES TO THE FILE. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASSDR VNAA2024051700009Skin · dentedL/H WING IB FLAP LOWER SKIN HAS SEVERAL DENTS. REMOVED DAMAGED SECTION OF SKIN. LOCATED AND INSTALLED NEW SECTION OF LOWER SKIN IAW REO 670-57-52-160 REV. A DATED 2016-10-21.SDR VNAA2024051700001Skin · dentedR/H INBOARD FLAP, LOWER SKIN HAS MULTIPLE DENTS. REPAIRED DAMAGE I.A.W. BOMBARDIER REO 670-57-52-160 REV.A, DATED 2016-10-21.SDR FDEA202405130661Skin · dentedRH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE, BETWEEN IFS 160.5 AND IFS 169 APPROX SKIN WITH DENTS. RH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 AND SRM 51-70-10-2R REP 2 FIG 203SDR FDEA202405130660Skin · gougedRH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE, BETWEEN IFS 220.5 AND IFS 206 APPROX SKIN WITH GOUGES. RH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 (SHEET 6) AND SRM 51-70-06-0G SDR ASAA2024051250248Bushing · wornL/H WING FIXED TRAILING EDGE FLAP TRACK ROLLER GUIDE UPPER SIDE HAS WORN FASTENER BUSHINGS (MARKED). GROUNDED - YES. REPAIRED L/H WING TRAILING EDGE FLAP TRACK ROLLER GUIDE UPPER SIDE / DEFLECTION CONTROL RIB UPPER TAB IAW B737-800 SRM 57-51-02-2R-4.SDR FDEA202405120645Skin · wornRH WING, OUTBOARD SLAT 8, TRAILING EDGE WEDGE, LOWER SURFACE AT OSS 433.71 APPROX, PREVIOUS REWORK DETERIORATED. RH WING OUTBOARD SLAT #8 TRAILING EDGE WEDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R REPAIR 1 NOTE B AND SRM 51-70-10-2R REPAIR 4 REV 88 DEC 15/SDR SWIA20240813511Skin · dentedRIGHT INBOARD FLAP LOWERE SKIN INBOARD OF THE INBOARD FLAP HINGE ARM HAS FOUR DENTS. (MARKED) (C-CHECK RO 8/11/2024) REPAIRED R/H I/B FLAP LOWER SKIN REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-803. SEE CONTINUATION SHEET FOR DETAILS. COMPLSDR FDEA202405100635Skin · dentedRH OB FLAP LWR SURFACE FOUND DENT AT 163 IN TO IB AND 9 IN TO AFT EDGE. EVALUATED RH OB FLAP LWR SURFACE DENT AT OTEF STA 197 DAMAGE SIZE LXW=2.6"X1.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2 REV 46.1. REPAIRED AS PER B777 SRMSDR DALA2024051305150Skin · dentedSHIP 190 RH WING I/B TRAILING EDGE AFT FLAP UPPER SKIN PANEL DENT FROM THE O/B END 26 INCHES, FROM THE TRAILING EDGE 15 INCHES. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 (0333951)SDR DALA2024051305149Skin · dentedSHIP 190 RH WING I/B TRAILING EDGE AFT FLAP UPPER SKIN PANEL DENT FROM THE O/B END 25 INCHES, FROM THE TRAILING EDGE 2 INCHES. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-2 (0333945)SDR DALA2024051305148Skin · dentedSHIP 190 RH WING I/B TRAILING EDGE AFT FLAP UPPER SKIN PANEL DENT FROM THE O/B END 15 INCHES, FROM THE TRAILING EDGE 2 INCHES. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-2 (0333937)SDR DALA2024051305147Skin · dentedSHIP 190 RH WING I/B TRAILING EDGE AFT FLAP UPPER SKIN PANEL DENT FROM I/B END 23 INCHES, FROM TRAILING EDGE 8 INCHES. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 (0333930)SDR DALA2024051305146Skin · dentedSHIP 190 RH WING I/B TRAILING EDGE AFT FLAP UPPER SKIN PANEL DENT FROM THE O/B END 12 INCHES, FROM THE TRAILING EDGE 10 INCHES. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 (0333864)SDR UIEA2024050800350Skin · wornWORN - SKIN LH OTBD FORE FLAP RH TOP PANEL FASTENER HOLE, FROM LH EDGE 18" AND FROM AFT EDGE 0.5"(<P>1) PERFORM REPAIR OF WORN SKIN DAMAGE AT LH WING OTBD FORE FLAP UPPER SKIN PANEL ASSY (PN 65B01915-427) IAW EGAT EI T2024A57M-838 REV 1. 2) CONDITION CHECK IS SDR DALA2024051005103Housing · corrodedSHIP 3119 CORROSION FOUND IN TRACK 2 BEARING HOUSING AT RIB 9 LEVEL ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 612951-14. (0334300)SDR FDEA202405080610Skin · crackedLEFT WING - INBOARD FLAP OUTBOARD LOWER SEGMENT UPPER SURFACE SKIN AT XIFH 249.5 FOUND CRACK ABOUT 1 INCH. LEFT WING - INBOARD FLAP OUTBOARD LOWER SEGMENT UPPER SURFACE SKIN CRACK AT XIFH 249.5 REPAIR CARRIED OUT AS PER EA 1-5750-T0379218 P1 TITLE - WINGS SDR SWAA2024052983158Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS266 AT RT WING 2024-293935<[01] REPLACED ANGLE LOCATED TRAILING EDGE LOCATED ORSS266 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930 SHEET 8 REV -.;[02] REPLACED ANGLE LOCATED TRAILING EDGE LOCATED ORSS266 AT RT WINGSDR SWAA2024050782959Panel · crackedPANEL 561AB CRACKED. LOCATED AND DRILLED NEW PANEL PER SRM 51-40-05. INSTALLED REPLACEMENT PANEL PER AMM 57-50-02 CLEARANCE CHECK GOOD.SDR SWAA2024052982818Web · crackedCRACK WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING. REPLACED WEB AND FASTENERS ON TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 115A 2512 SHEET 14; REV. A.SDR AALA202405291495Trunnion · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP TRUNNION WORN AT RIB 1 AND WXO. REPLACED FLAP TRUNNION PER TASK CARD 26L00027003.SDR SBOY202405080001Shim · migratedFOUND OUTBOARD FLAP SUPPORT #8 WITH SHIM MIGRATION DURING SI IB777570078 INSPECTION.SDR SWAA2024050682426Skin · delaminatedR/H T/E AFT FLAP HAS DELAMINATION ON I/B SIDE<[01] R&R RH OUTBOARD AFT FLAP PER AMM 27-51-22.;[02] VERIFIED R&R / INSTALLATION AND ADJUSTMENT OF RIGHT OUTBOARD AFT FLAP ASSEMBLY PER AMM 27-51-22-400-801SDR AALA202405063993Skin · puncturedAIRCRAFT WAS GROUNDED: LEFT WING INBOARD FLAP HAS A PUNCTURE AT WS 204. REPAIRED FLAP PER EA 350164A AND SRM 51-70-10-2R-2.SDR SWAA2024050682044Skin · delaminatedR/H OUTBOARD TRAILING EDGE FLAP HAS DELAMINATION FOUND ON INBD SIDE<[01] REF BARCODE TTG8Q00T4FGT. C/W EA 24-127-01188SDR FDEA202405030567Skin · dentedREWORK NR N00056 LH WING OUTBOARD FLAP LOWER SURFACE WITH DENT AT 10" FROM LOWER EDGE AND 61" FROM INBOARD FAIRING FLAP REWORK WAS PERFORMED NR N00056 ON LH WING OUTBOARD FLAP LOWER SURFACE AT 10" FROM LOWER EDGE AND 61" FROM INBOARD FAIRING FLAP IAW B767 SDR AALA202408283314Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE OUTBOARD FLAP INTERNAL SUPPORT AT FLAP TRACK 4 AND FLAP RIB 14 INBOARD SIDE. REPLACED FLAP PER TASK CARD 26L00027009.SDR AALA202408287773Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE OUTBOARD FLAP INTERNAL SUPPORT AT FLAP TRACK 4 AND FLAP RIB 15 OUTBOARD SIDE. REPLACED FLAP PER TASK CARD 26L00027009.SDR SWAA2024061781481Skin · debondedDEBONDED O/B AFT FLAP ON LOWER SURFACE IB SIDE AT RT WING. PERFORMED INTERIM REPAIR ON O/B AFT FLAP AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTIONS EVERY 6;875 FC OR 30 MONTHS WHICHEVER COME FIRST.SDR SWI20240515000411Vane · damagedLH WING IB FLAP MOVEABLE VANE HAS CHAFFING DAMAGE WHERE THE VANE MEETS THE STOPS IN THREE SPOTS. (C-CHECK RO 5/14/2024) PERFORMED TEMPORARY REPAIR OF THREE AREAS OF CHAFING DAMAGE TO THE LH IB FLAP VANE IN REF TO REO 601R-57-52-004, REV D, DATED 2012-12-1SDR SWI20240515000410Vane · chafedRH WING IB FLAP MOVEABLE VANE HAS CHAFFING DAMAGE WHERE THE VANE MEETS THE STOPS IN THREE SPOTS. (C-CHECK RO 5/14/2024) PERFORMED TEMPORARY REPAIR OF THREE AREAS OF CHAFING DAMAGE TO THE RH IB FLAP VANE IN REF TO REO 601R-57-52-004, REV D, DATED 2012-12-1SDR IPXA2024051044954Bolt · shearedRH O/B FLAP I/B HINGE FWD BOLT IS BROKEN ATA 57-55. VERIFIED REMOVED AND REPLACED R/H O/B FLAP I/B FWD HINGE BOLT P/N ARC0882-501 BATCH: 0004096187 IN REF TO UPS MD11 AMM 57-53-01-400-801 TW ID:19-411 CAL DUE: 16-AUG-2024.SDR SWAA2024052980593Fairing · delaminatedNUMBER 5 FLAP TRACK AFT FAIRING PANEL 194BR, FWR LWR CORNER DELAMINATED. APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL 194BR IAW SRM 51-70-04-2R-13 PARAG 4-D-G. .APPLIED TOP COAT AT PANEL 194BR IAW AMM 51-21-99-300-802.SDR SWAA2024052980592Panel · damagedRIGHT WING I/B #5 FLAP TRACK PANEL 3194CR; ELONGATED FASTENER HOLES NOTED. APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #194CB AS PER B737 SRM 51-70-04-2R-9 PARAG 4-D-G. APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #194CR IAW SDR SWAA2024051680242Skin · delaminatedRIGHT INBOARD FLAP OUTBOARD FLAP OUBOARD LOWER SURFACE HAS DELAMINATION<[01] REMOVED AND REPLACED RH I/B FLAP O/B FLAP LOWER SURFACE PART IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DWG 113A2100 REV. -;[02] VERIFIED STDP 1 JOB IS COMPLETE.<BR>AUDIT C/W.SDR SWAA2024051680243Skin · delaminatedLEFT WING OUTBOARD FLAP AFT FLAP LOWER SURFACE INBOARD CORNER IS DELAMINATED<[01] 04 - REPAIRED PER [SRM 57-53-01-2R-16-B01475 (REPAIR 16 - OUTBOARD AFT FLAP TRAILING EDGE WEDGE ASSEMBLY REPAIR - PERMANENT)];[02] AUDIT C/WSDR SWAA2024051680247Skin · delaminatedRIGHT WING OUTBOARD FLAP INBOARD LOWER CORNER OF AFTFLAP IS DELAMINATED<[01] REPAIRED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16 AND SRM 51-70-10-2R-0 REPAIR GENERAL.;[02] AUDIT C/WSDR IPXA2024052211513Support Fitting · corrodedFOUND CORROSION ON R/H SIDE SUPPORT FOR O/B FLAP I/B FWD FLAP HINGE ATA 57-55 REMOVE AND REPLACE SUPPORT P/N ARB0029-510 PER MD11 AMM 57-53-01-400-801 AND SRM 51-30 REQUIREMENTS.SDR SWAA2024052280123Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP I/B EDGE LOWER SIDE DELAMINATED.<[01] REMOVED FLAP.;[02] REMOVED AND REPLACED R/H O/B AFT FLAP PER AMM 27-51-22. SEE STEP 1 FOR WORK ACCOMPLISHED.;[03] RII INSPECTION C/W FOR R/H O/B AFT FLAP ADJUSTMENT CHECK GOOD PER AMM 27-51-22 SDR SWAA2024043079815Fairing · crackedLEFT WING #1 FWD FLAP SUPPORT FAIRING INBOARD SIDE HAS A 2.6' LONG CRACK; 12' FROM FWD EDGE AND 4' FROM TOP SURFACE LEFT WING #1 FWD FLAP SUPPORT FAIRING INBOARD SIDE HAS A 2.6' LONG CRACK 12' FROM FWD EDGE AND 4' FROM TOP SURFACE<[01] PERFORMED REPAIR ON #1 LSDR UIEA2024042400307Skin · dentedRH WING OUTBOARD FLAP INNER SURFACE FWD SECOND BAY STA 622 APPROX WITH TWO DENTS(<P>DENTS (2 EA) ON RH WING OUTBOARD FLAP INNER SKIN PANEL WERE REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400308Skin · dentedRH WING OUTBOARD FLAP INNER SURFACE FWD SECOND BAY STA 636 WITH DENT(<P>DENT ON RH WING OUTBOARD FLAP INNER SKIN LOWER PANEL AT OTEF 101.73 WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400315Skin · delaminatedLH WING, INBOARD FLAP SURFACE INNER SIDE AREA AFT FLAP OUTSIDE CORNER WITH DELAMINATION(<P>DELAMINATION ON LH WING INBOARD AFT FLAP LOWER SURFACE WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)
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