JASC 5753
Service difficulty reports · 31,515
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 UPS07M49673Stop Fitting · crackedINSPECTION TYPE:C LT WING O/B FLAP MID STOP FITTING FOUND WITH CRACK AS MARKED. LHW O/B FLAP I/B AND O/B HINGE ASSY, CARRIAGE, VANE TRACK AND HINGE FAIRING SUPPORT REMOVED PER CMM 57-52-04 R.57 AND SRM 51-31-01 V.II R.38 SEND OUT FOR REPAIR. LHW OB FLAP IB ASDR ASAA0741441Skin · puncturedRIGHT WING NR 6 SPOILER SURFACE IS PUNCTURED 8 INCHES FROM THE T/E, 12 INCHES FROM THE O/B EDGE (UPPER SURFACE). PREPPED THE DAMAGED AREA OF UPPER SKIN FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2.SDR ASAA0741439Skin · puncturedTHE RIGHT WING O/B FORE FLAP IS PUNCTURED ON THE LWR SURFACE NEAR THE I/B END. REMOVED DAMAGED AREA OF LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 APRA 7, 11, 15, 18 AND 20.SDR USAA070080Skin · chafedOUTBOARD END OF LEFT WING OUTBOARD MID FLAP CHAFED. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-53-03, DEFECT SIZE: 1 X 2 INCHES.SDR 07FDEA00324Skin · damagedOLD REPAIR ON LT INBOARD FLAP ON TOP SKIN CLOSE TO TRACK 2 RIB 7. REPAIR WAS PERFORMED IAW RAS/FOK/064/2003 ISSUE B.SDR 07FDEA00304Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107781 PT1, REPAISDR 07FDEA00303Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107781 PT1, RESDR 07FDEA00302Hinge · corrodedRIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED.SDR 07FDEA00301Hinge · corrodedRIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107780 PT1, SDR DHL2007802528Vane · misrepairedRT OTBD SLOT VANE HAS A NON STANDARD REPAIR STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-57-106 REV IR DATED 01-22-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGESDR DHL2007802521Vane · misrepairedLT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG AC62-57-108 REV IR DATED 01-23-07. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SSDR 07FDEA00265Rib · crackedOLD REPAIR ON RT INNER FLAP RIB 25 CRACK FINDING (3, 5 INCHES) DURING SB A300-57-6098 EMBODIMENT REPAIR WAS PERFORMED WITH CAL EO AB6-57-00-0063 AND APPROVED BY RAS/FOK/176/2004.SDR DHL2007802526Vane · misrepairedRT OTBD SLOT VANE HAS A NON STANDARD REPAIR, STA XS 512.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-07, DWG NR AC62-57-104 REV A DATED 01-31-07. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DASDR UIEA200700064Flap Track · gougedNR 5 FLAP TRACK FORWARD FITTING OUTBOARD SURFACE FOUND WITH GOUGE. REPAIRED GOUGED AREA, BLENDED AND SMOOTHED PER SRM 51-10-00. DETAIL VISUAL AND HFEC INSPECTED. FOUND NO DEFECTS. AREA PROTECTED AND PAINTED. FOUND WITHIN SERVICEABLE LIMITS.SDR 07FDEA00247Skin · delaminatedREPAIR FOUND ON THE RT OB AFT FLAP LOWER SURFACE SKIN 17" FROM IB END REQUIRED EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND TO BE OUT OF LIMITS. REPLACED AFT FLAP. NEW AFT FLAP INSTALLED ON SNSDR ASAA0741438Skin · dentedTHE RIGHT WING O/B AFT FLAP HAS A LARGE DENT JUST BELOW THE SECOND CARRIGE FROM THE O/B END. REMOVED THE DAMAGED AREA OF LWR SKIN AND CORE FABRICATED AND INSTALLED A CORE PLUG SKIN FILLER AND TWO REPAIR DOUBLERS IAW SRM 51-70-10 PARA 7, 8, 9, 11, 15, 18 AND 2SDR ASAA0741437Skin · dentedTHE LEFT WING I/B MIDFLAP T/E IS DENTED AND GOUGED AT THE AFT EDGE ON THE LWR SURFACE. PREPARED THE LWR SKIN FOR BONDING, APPLIED POTTING COMPOUND, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20.SDR SWAA070541Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E END. REMOVED AND REPLACED AFT FLAP PER MM.SDR IXXA07SMN087SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL HAS A NON STANDARD REPAIR FROM STATION XF169.000 TO STATION XF172.000. REMOVED EXISTING SKIN PANEL WITH NON STANDARD REPAIR. FABRICATED NEW SKIN PANEL AND REPAIR PARTS. BONDESDR IXXA07SMN065SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF240.000. REMOVED EXISTING REPAIR. REMOVED DAMAGED SKIN. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED NEW SKIN ANSDR FXG2007F00000Bracket · brokenAFTER FLIGHT MAINTENANCE FOUND THE OB ATTACH BRACKET AT THE OB END OF FLAP ASSY 5363998-501 BROKEN. THIS ALLOWED THE VANE ASSY 5371802-1 TO COME LOOSE AND DAMAGE THE FLAP. REPLACE THE FLAP AND VANE ASSY. RETURNED AC TO SERVICE. (K)SDR IXXA07SMN064SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND UPPER OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF210.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN AS NEEDED. APPLIED SEALANTSDR IXXA07SMN073SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING FLAP UPPER SKIN HAS A NON STANDARD REPAIR BETWEEN STATIONS XF415.000 AND XF420.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNASDR IXXA07SMN063SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER OUTBOARD FLAP CRACKED AT STATION XF442.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND REPAIR PARTS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA, NEW SKIN AND REPAIR PARTS AS NSDR A6WA200740039Flap System · jammedON APPROACH INTO YOW, FLAPS FAIL CAS MESSAGE FAILED AT 0 DEGREES, COMPLIED WITH QRH. LANDED AT APPROXIMATELY 40,600 LBS, CREW DID NOT CALL IN DISCREPANCY. NO HES/RTO INSPECTION REQUIRED. INTERROGATED FECU, FECU SHOWS FLAP FAIL WAS DUE TO JAM ON LEFT WING. SDR IXXA07SMN066SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER OUTBOARD FLAP HAS A NON STANDARD REPAIR AT STATION XF350.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND NEW SKIN AS NEEDED. APPLIED SEALANT SDR SWAA070531Torque Tube · corrodedDURING SCHEDULED 22Y CHECK, FOUND LEFT INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA070530Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD T/E DELMAINATED. REPAIRED MID FLAP PER SRM.SDR SWAA070499Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD AFT FLAP DELAMINATED AT INBOARD FLAP TRACK. REMOVED AND REPLACED AFT FLAP PER MM.SDR 07FDEA00216Skin · unknownRT WING I/B FLAP LOWER SKIN FWD I/B OF HINGE AT STA XIFH 255, EXISTING DOUBLER REPAIR. NEW REPAIR INSTALLED IAW SRM 57-10-00 FIG 86 VOL 1. RUB STRIP INSTALLED IAW DWG ARC3007. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01106 AND SRM 57-10-00 VOL1 FIG 86 ANDSDR DHL2007781017Structure · crackedFOUND LT IB MID FLAP WBL 71-134 HAS 4 CRACKS ON 3 CUTOUTS ON THE AFT LOWER CHORD. REMOVED DAMAGED SECTION OF AFT LOWER CHORD APPROX 70 3/8. LOCATED AND DRILLED NEW CHORD P/N BAC1503-100046 PO NR 652296 DIM 70 3/8 IAW B727 SRM 57-50-2 FIG 5, 51-40-4 FIG 1 ANDSDR UIEA200700041Bearing · migratedLT WING NR 3 FLAP TRACK FWD ATTACH FITTING BEARING FOUND MIGRATION. REPAIRED ACCOMPLISHED AS PER SB747-57-2325.SDR UIEA200700042Bearing · migratedRT WING NR 6 FLAP TRACK FWD ATTACH FITTING BEARING FOUND MIGRATED. REPAIRED ACCOMPLISHED AS PER SB747-57-2325.SDR SWAA070482Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR NWAA070689885Stringer · crackedDURING "H" CHECK, FOUND CRACK IN LT WING TRAILING EDGE FLAP FORWARD SPAR UPPER STRINGER. REPAIRED PER EA 99-208451.SDR SWIA200717767Bearing · malfunctionedOUTBOARD FLAPS WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO FIELD. REPLACED 4 ROLLER BEARINGS IAW MM 27-50-12. OPERATIONAL CHECKS GOOD IAW MM 27-50-00.SDR ASAA0741421Skin · chafedRIGHT O/B FORE FLAP L EADING EDGE CHAFED. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-53-01 FIG 201 REPAIR 1.SDR ASAA0741420Skin · delaminatedRIGHT I/B AFT FLAP IS DELAMINATED ON O/B EDGE LOWER SURFACE. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER IAW SRM 51-70-10.SDR DHL2007802517Frame · crackedFOUND LT OTBD FLAP FORMER 1.500" CRACKED STA XF 165.000. REMOVED CRACKED FORMER IAW SRM 51-1-21. FABRICATED NEW FORMER (AL7075"0" 0.050") IAW SRM 57-2-0 PG 1. HEAT TREATED FORMER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 13-17. CLEANED, TREATED AND PRIMED FSDR SWAA070423Wedge · debondedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD MID FLAP T/E WEDGE LOWER T/E OUTBOARD END DISBONDED. REPAIRED MID FLAP PER SRM.SDR COMA0760094Shaft · damagedFLIGHT 5145 - RECEIVED FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE NR 4 FLEX DRIVE SHAFT.SDR COMA0760069Shaft · damagedFLIGHT 5164 - FLAP FAIL MESSAGE RECEIVED ON APPROACH AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 LEFT WING FLEX SHAFT.SDR COMA0760068Shaft · damagedFLIGHT 5164 - FLAP FAIL MESSAGE RECEIVED ON APPROACH AT ZERO DEGREES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 LEFT WING FLEX SHAFT.SDR COMA0760065Shaft · bentFLIGHT 5564 - RECEIVED FLAP FAIL MESSAGE AT ZERO DEGREES ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE FLEX SHAFTS NR 3.SDR UPS07M49556Skin · dentedINSPECTION TYPE: C RE SKIN LEFT I/B FLAP AFT I/B & O/B SEGMENT DUE MULTIPLE DENTS. REMOVED LEFT WING I/B FLAP SPRING CARTRIDGE PER AMM27-51-04 R55. REMOVED I/B FLAP O/B AFT SEGMENT PER AMM20-50-02 R55. LEFT WING I/B FLAP & O/B SEGMENT LWR SKIN REMOVED PER SSDR UPS07M49555Skin · dentedINSPECTION TYPE:C RE SKIN I/B FLAP LOWER AFT I/B AND O/B SEGMENTS DUE MULTIPLE DENTS. REMOVED RIGHT WING I/B FLAP CARTRIDGE PER AMM27-51-04 R55. REMOVED BOTH I/B AND O/B SEGMENT PER AMM20-50-02. RIGHT WING FLAP LWR I/B & O/B SEGMENT SKIN REMOVED PER SRM 51-SDR AWXA200700223Skin · delaminatedMCN - FOUND RIGHT WING INBOARD FOREFLAP UPPER SKIN DELAMINATED, WBL 181. REPAIRED RIGHT WING INBOARD FOREFLAP UPPER SKIN, WBL 181 IAW B737-300 SRM 51-70-10.SDR AWXA200700202Skin · delaminatedMCN - FOUND RIGHT WING OUTBOARD AFT FLAP LOWER SKIN HAS AREA OF DELAMINATION, WS 248.10 - WS 251.40, 19" FROM INBOARD EDGE. REPAIRED RIGHT WING OUTBOARD AFT FLAP LOWER SKIN WS 248.10 - WS 251.40, 19" FROM INBOARD EDGE IAW B737-300 SRM 51-70-10-2R3.SDR SWAA070374Flap · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT T/E OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA070371Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM.
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