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 ASAA2024071152133Spar · corrodedR/W I/B FLAP, REAR SPAR HAS CORRSION ON LOWER LEG INNER SURFACE. GROUNDED - YES. EVALUATED CORROSION, FOUND TO BE 100% MATERIAL LOSS. AREA #1, TRIMMOUT CORROSION 44.45 X 19.05MM, AREA #2 TRIM OUT 21.08MM X 19.05MM, AREA #3 TRIMOUT 21.08MM X 19.05MM, AREA #4 RESDR FDEA202407111003Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPPER SKIN BETWEEN RIB16~17, S2.1~S2.2 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRSDR DALA2024071207089Bearing · corrodedSHIP 3124 CORROSION LH WING INB FLAP TRACK 2 BEARING AT RIB 9 LEVEL / INB & OUTB PLATES. CORRECTIVE ACTION: REPAIRED PER ER/A 614887-14. (0441615)SDR VNAA202409010002Skin · nickedSEVERAL 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 65.5 AT RH WING WAS BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01, BTW FLS 45.00 TO FLS 65.5 WAS EVALUATED WITHIN LMIMITS PER CSDR SWI2024F00600Flap Track · damagedL/H FLAP TRACK #2A OUTBOARD HAS WIDTH REDUCTION DAMAGE WITH A MAXIMUM LOSS OF .40 MM. TC2-8916 CAL DUE 11-20-24. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED LH #2A OB FLAP TRACK REF EMB AMM 57-54-25-400-801-A TW: TC2-7543 CAL DUE: 05/13/2025SDR UIEA2024071000602Skin · debondedDISBOND - SKIN, 4H WING INBD MID FLAP EXTERNAL LWR SURFACE.(<P>1. PERFORM DISBOND SKIN PERMANENT REPAIR AT 4H WING INBD MID FLAP LWR SURFACE IAW JOB CARD ATTACHING SHEET NO 0391716, 0407121, 0407120 FOR DETAILED PROCESS AND EGAT EI NO T2024A57M-1397 REV 1 2. CSDR UIEA2024071000613Bushing · corrodedFOUND NO. 1 TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION.(<P>1. REFENCE TO EI NO: T2024A57M-1462 REV 1 SEQUENCE A. REPLACE BUSHING 2. CONDITION CHECK NORMAL</P>)SDR UIEA2024071000614Bushing · corrodedFOUND NO. 7 TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION.(<P>1.3 REFERENCE EI NO: T2024A57M-1466 REV 1 SEQUENCE A. REPLACE BUSHING 2. CONDITION CHECK NORMAL.</P>)SDR UIEA2024071000615Bushing · corrodedFOUND NO. 6 TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION.(<P>1. REFERENCE EI NO: T2024A57M-1465 REV 1 SEQUENCE A REPLACE BUSHING 2. CONDITION CHECK NORMAL.</P>)SDR UIEA2024071000616Bushing · corrodedFOUND NO. 3 TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION.(<P>1. REFERENCE EI NO: T2024A57M-1464 REV 1 SEQUENCE A. REPLACE BUSHING 2. CONDITION CHECK NORMAL.</P>)SDR UIEA2024071000617Bushing · corrodedFOUND NO. 2 TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION.(<P>1. REFERENCE EI NO: T2024A57M-1463 REV 1 SEQUENCE A. REPLACE BUSHING 2. CONDITION CHECK NORMAL.</P>)SDR UIEA2024071000618Bushing · corrodedFOUND NO. 8 TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION.(<P>1. REFERENCE EI NO: T2024A57M-1467 REV 1 SEQUENCE A. REPLACE BUSHING 2. CONDITION CHECK NORMAL.</P>)SDR AALA202408021758Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING INBOARD TRAILING EDGE FLAP OUTBOARD SIDE INTERCONNECTIING STRUT LOWER ATTACHMENT FITTING / BRACKET WHICH CAUSED EXCESSIVE BEARING PLAY AT RIB 14. REPLACED ATTACHMENT FITTING / BRACKET PER SRM 51-42-11.SDR AALA202408028274Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD TRAILING EDGE FLAP OUTBOARD SIDE INTERCONNECTIING STRUT LOWER ATTACHMENT FITTING / BRACKET WHICH CAUSED EXCESSIVE BEARING PLAY AT RIB 14. REPLACED ATTACHMENT FITTING / BRACKET PER SRM 51-42-11.SDR FDEA202407080971Skin · delaminatedLEFT WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION AT 60" FROM OUTBOARD FITTING NO 1. LEFT WING OUTBOARD FLAP LEADING EDGE AT 60" FROM OUTBOARD FITTING NO 1 WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE I AND SRM 51-70-03-0G PAR 5.A FIG 9 REV 88 DEC 15SDR DALA2024070806927Bonding Plate · brokenSHIP 3132 BROKEN BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WIN. CORRECTIVE ACTION: REPAIRED PER ER/A 618279-14. (0435053)SDR SWAA2024072910162Skin · delaminatedRIGHT HAND I/B MAIN FLAP LOWER O/B SURFACE SHOWS EVIDENCE OF DELAMINATION. (MARKED)<[01] REMOVED DAMAGE TO AREA PER SRM 51-70-10-2R-0.;[02] VERIFIED REMOVAL OF DAMAGE TO AREA PER SRM 51-70-10-2R-0.;[03] ACCOMPLISHED PERMANENT REPAIR TO R/H MAIN FLAP T/E WEDGE SDR SWAA2024072910170Skin · delaminatedL/H INBD AFT FLAP HAS DELAMINATION ON OBD SIDE & SPLIT TRAILING EDGE.<[01] OK TO INSTALL NEW WEDGE.;[02] THIS CARD IS WRITTEN IN ERROR. IT IS A DUPLICATE WRITEUP OF TTG8Q00UEC70.;[03] THIS CARD IS WRITTEN IN ERROR. IT IS A DUPLICATE WRITEUP OF TTG8Q00UEC70.;[0SDR SWAA2024071910146Fairing · damaged#6 INBOARD FLAP SUPPORT AFT FAIRING TAIL CONE HAS PULLED FASTENER<[01] REMOVED AND INSTALLED SERVICEABLE RIGHT WING #6 AFT SUPPORT FAIRING TAIL CONE PER. M.M. 27-51-18SDR UIEA2024070300574Skin · delaminatedDELAMINATION ON LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE(<P>LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 2 AND 51-70-03-0G-0 PAR 5A , 25 REV 125 APR 15/2024. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024070400577Skin · delaminatedDELAMINATION ON LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE(<P>LEFT WING, INBOARD MAIN FLAP, LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 2 AND 51-70-03-0G-0 PAR 5A , 25 REV 125 APR 15/2024. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024070806928Pendulum · corrodedSHIP 3132 CORROSION ON PENDULUM TRACK 2 I/B FLAP ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 618466-14. (0432955)SDR SWI2024F00598Flap Track · wornWIDTH REDUCTION OF APPROXIMATELY 1.2MM ON RH OB FLAP TRACK #2A. ASSET: TC2-8911 DUE:11-8-24 (C-CHECK RO 7/22/2024) FOUND RH OB FLAP TRACK #2A TO BE OUT OF LIMITS. REMOVED AND REPLACED RH OB FLAP TRACK #2A WITH REF TO AMM 57-54-25. ASSET# TC2-7520 CAL DSDR DALA2024070806910Bonding Plate · corrodedSHIP 3137 DEBONDED FLAP TRACK FAIRING 633CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618290-14. (0430554)SDR DALA2024070806909Bonding Plate · corrodedSHIP 3137 CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618290-14. (0430551)SDR DALA2024070806908Bonding Plate · corrodedSHIP 3137 CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618290-14. (0430548)SDR DALA2024070806907Bonding Plate · corrodedSHIP 3137 CORROSION FLAP TRACK FAIRING 631CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618290-14. (0430547)SDR DALA2024070806906Bonding Plate · corrodedSHIP 3132 CORROSION BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618279-14 REV. ORIGINAL. (0429769)SDR DALA2024070806905Bonding Plate · corrodedSHIP 3140 CORROSION BONDING PLATE FLAP TRACK FAIRING 4 ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618277-14. (0430950)SDR DALA2024070806904Bonding Plate · corrodedSHIP 3140 CORROSION FLAP TRACK FAIRING 631CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618277-14. (0430946)SDR DALA2024070806903Bonding Plate · corrodedSHIP 3140 CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618277-14. (0430937)SDR DALA2024070806902Bonding Plate · corrodedSHIP 3140 CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 618277-14. (0430934)SDR FDEA202407050947Skin · delaminatedRH OUTBOARD FLAP LEADING EDGE LOWER SURFACE AT OTEF STA 47 APPROX SKIN WITH DELAMINATION. RH OUTBOARD FLAP LEADING EDGE LOWER SURFACE AT OTEF STA 47 APPROX SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 TABLE I PAG 1-5 AND SRM 51-70-03-0G PAR 5.A FIG 5 SDR DALA2024070806848Skin · dentedUPPER OB FLAP HAS MULTIPLE DENTS. INSTALLED MULTIPLE PERMANENT REPAIRS PER B767-400 SRM 57-53-01-2R.SDR AALA202408144406Bracket · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT FITTING AFT ATTACHMENT BRACKET WORN AT RIB 13 . REPLACED BRACKET PER SRM 51-42-11.SDR AALA202408063339Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP TAB LOWER SURFACE SKIN PREVIOUS REPAIR DEBONDING AT 12.5 INCHES FROM TRACK 3B AND 5.5 INCHES FROM THE FRONT SPAR. REPAIRED FLAP TAB PER SRM 57-53-00-300-107.SDR FDEA202407040933Skin · delaminatedLH WING OB FLAP UPR SURFACE FROM IB TO OB 93 INCH CROSS TE TO LE 12 INCH FOUND PREVIOUS REPAIR . REDID LH WING OB FLAP UPR SURFACE FROM IB TO OB 93 INCH CROSS TE TO LE 12 INCH PREVIOUS REPAIR AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R RPAIR SDR FDEA202407040932Skin · delaminatedLH WING OB FLAP LWR SURFACE FROM IB TO OB 93 INCH CROSS TE TO LE 7.5 INCH FOUND PREVIOUS REPAIR. REDID LH WING OB FLAP LWR SURFACE FROM IB TO OB 93 INCH CROSS TE TO LE 7.5 INCH PREVIOUS REPAIR AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R RPAIR SDR SWIA2024091607003Doubler · damagedUPON REMOVAL OF STUCK SCREWS, FOUND 2EA MISDRILLED HOLES IN PANEL 591FT STRUCTURE. CAMP 28475622 (C-CHECK RO 9/15/2024) REPAIRED 2EA ELONGATED HOLES TO LH OUTBOARD FLAP LOWER DOUBLER BETWEEN FLAP STA 209.390 - FLAP STA 226.150 PER REO 690-57-53-158 REV SDR COEA2024080226738Skin · chafedLEFT WING FLAP UPPER SURFACE AFT OF THE ENGINE NACELLE IS CHAFED. REPAIRED IAW TEXTRON DQ44948M1 DATED 7/16/2024.SDR SWAA2024071809065Skin · delaminatedRH WING: O/B AFT FLAP; UPPER SURFACE DELAMINATED; 4 INCHES FROM T/E AND 3 INCHES I/B END.<[01] RH WING O/B AFT FLAP TO BE REPLACED ON FAULT#TTG8Q00UCWET.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR HNAA2024091200783Angle · corroded57-2177 - RH WING INBD FLAP LOWER SKIN, ROOT SPARE ANGLE CORRODED.SDR SWAA2024072308228Skin · delaminatedL/H WING O/B AFT FLAP DELAMINATED AT I/B END LOWER SURFACE<[01] OK TO INSTALL L/H O/B AFT FLAP.;[02] L/H O/B AFT FLAP INSTALLED TO STEP 'G. OUTBOARD AFT FLAP ADJUSTMENT'; IAW AMM 27-51-22;[03] CORRECTION: L/H O/B AFT FLAP INSTALLED THROUGH STEP '3. F. (5) (G)'SDR AALA202407080883Strut · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO LAX DUE TO THE FLIGHT CREW REPORTING A FLIGHT CONTROL FLAPS LOCKED MESSAGE WITH THE FLAPS JAMMED AT POSITION 1. AIRCRAFT LANDED AFELY AT LAX WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR ASDR DALA2024070306734Fairing · corrodedCORROSION FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. REPAIRED PER ER/A 618277-14.SDR SWAA2024070308042Skin · delaminatedR/H O/B FLAP TRAILING EDGE FLAP DELAMINATED I/B CORNER.<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP - REMOVAL/INSTALLATION - PERMANENT)<BR>OPS CHECK GOOD.SDR DALA2024070206694Track · corrodedSHIP 3132 CORROSION PENDULUM TRACK 3 O/B FLAP RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 618088-14 REV. ORIGINAL.SDR SWAA2024072907793Skin · delaminatedLH OUTBD AFT FLAP LOWER INBD CORNER HAS DELAMINATION ON UPPER AND LOWER SURFACES.<[01] OK TO INSTALL L/H OUTBD AFT FLAP.;[02] OK TO INSTALL AFT OUTBD FLAP;[03] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22.;[04] INSTALLED NEW SERVICEABLE L/H O/B SDR FDEA202406300885Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB11, RIB13 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB11, RIB13 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FLSDR FDEA202406300884Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB17, RIB18, RIB20 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17, RIB18, RIB20 BETWEEN STGR2.8 AND REAR SPAR. TIT
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