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 08FDEA03964Skin · chafedFOUND 2 AREAS OF CHAFING MARKS ON LT OUTER FLAP TOP SKIN, RIB 4-5 AND 15-17. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/227/2008 ISS A, APPROVED BY EA 6-5754-123065.SDR 08FDEA03963Skin · chafedFOUND 2 AREAS OF CHAFING MARKS ON RT SLAT NR 1 LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/234/2008 ISS A, APPROVED BY EA 6-5742-123083.SDR 08FDEA03960Skin · chafedFOUND CHAFING MARKS ON RT CENTER FLAP TOP SKIN RIB 13-15 AND 20-21. REPAIR PERFORMED BY CUT OUT THE SKIN AREA AND CHAFING PLATE AT RIB 13-13A AND INSTALL AN EXTERNAL DOUBLER AND A NEW CHAFING PLATE, BLEND OUT CHAFING MARK AT RIB 20-21 AND INSTALL A NEW CHAFSDR USAA920081737Wedge · delaminatedMAJOR REPAIR, RT WING INBOARD MIDFLAP TRAILING EDGE WEDGE DELAMINATED AT WBL 108.5 THRU WBL 111.5. REPAIRED RT WING INBOARD MIDFLAP TRAILING EDGE WEDGE AT WBL 108.5 THRU 111.5 IAW 51-70-10-2R4.SDR CA081009002Switch · damaged(CAN) THE FLAP SWITCH SHOULD SPRING BACK TO OFF POSITION WHEN PRESSURE IS RELEASED. THE PILOT SELECTED 20° OF FLAP TOOK PRESSURE OFF SWITCH BUT THE FLAPS EXTENDED TO 40° NEW SWITCH INSTALLED.SDR ASAA0843608Skin · chafedLT WING O/B MID FLAP LOWER SURFACE CHAFED O/B OF NR 1 FLAP TRACK. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 PG 254.SDR 08FDEA04339Skin · gougedFLAP INBD RT UPPER SKIN AT FLAP ZONE OF RIB 1 BETWEEN STR 2.1 / STR 2.2 WITH SMALL GOUGE WAS REPAIRED IAW EA 6-5710-121707 AND SRM 57-50-00.SDR 2008UALA05785Wedge · debondedFOUND LEFT INBD MID FLAP TRAILING EDGE WEDGE DISBONDED BETWEEN THE WEDGE AND ATTACH CHANNEL. GAP BETWEEN TRAILING EDGE WEDGE OF MID FLAP AND LEADING EDGE OF AFT FLAP IS OUT OF LIMITS. REMOVED T/E WEDGE & ADJUSTED GAP. REPLACED MID FLAP WEDGE. REPLACED INBD TESDR 08FDEA03942Wedge · crackedLEFT INBD FLAP, INBD TRAILING EDGE IS CRACKED. REMOVED TRAILING EDGE SECTION IAW SRM 51-35-02. FABRICATED IAW SRM 57-20-00. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-02.SDR SWAA085117Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR ASAA0843606Skin · chafedRT WING O/B FORE FLAP I/B LEADING EDGE CHAFED FROM CONTACT WITH CAVITY PANEL. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND DOUBLER IAW B737 400 SRM 51 53 01 FIG 201 AND INSTALLED.SDR DHLA2008745515Rib · corrodedRIGHT I/B MID-FLAP O/B RIB AT RWBL 133 CORRODED. REMOVED AND REPLACED RIB SECTION BY FABRICATION IAW B727 SRM 51-10-1 AND 51-30-2.SDR SWAA085113Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR 08FDEA04390Skin · damagedRT WING, INBD FLAP WITH ACCESS HOLE AT RIB 7 OVER DIMENSIONAL AT INNER LOWER SKIN SURFACE, IT WAS REPAIRED IAW EA 6-5750-121702.SDR ASAA0843599Skin · dentedRT WING AFT I/B TRAILING EDGE FLAP LOWER SURFACE DENTED IN 4 SPOTS. REMOVED DAMAGED SKIN, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR 08FDEA04338Spar · wornLEFT WING FLAP INBD W/ HOLES OVALIZED AT FRONT SPAR OF RIB 7 THE FRONT SPAR WAS REPAIRED IAW EA 6-5750-121702.SDR 08FDEA03869Skin · chafedLEFT WING INBD FLAP TOP SKIN IS CHAFED AT APPROX 13 INCHES AFT OF THE FRONT SPAR AND 79 INCHES FROM THE INBD EDGE. BLENDED CHAFED AREA REF SRM SRM 51-73-10. ORIGINAL MATERIAL THICKNESS 0.031 REF SRM 57-52-12. REMOVED MATERIAL 0.003. MATERIAL REMAINING 0.02SDR 2008UALA05694Skin · damagedLEFT OUTBOARD FLAP 12 INCHES LONG BY 5 INCHES WIDTH BY THREE EIGHTS INCH DEEP. APPROXIMATELY 13FT 3 INCHES FROM O/B EDGE OF O/B END OF FLAP. REPLACED LT OTBD FLAP. COMPLETED INSP OF FLAP INSTALLATION, ADJUSTMENT AND OPS.
SDR USAABB08151Bearing · damagedPHL FLT 734 EN-ROUTE PHL TO MAN. DURING CLIMBOUT FROM PHL, THE CREW RECEIVED AN ASYMMETRICAL TRAILING EDGE FLAP DISAGREE MESSAGE. THE CREW DECIDED TO RETURN TO FIELD IN PHL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A LEFT WING OUTSDR CA080918002A/C Pack · broken(CAN) DURING C-CHECK INSPECTION (1C, 2C, 4C, CPCP2, A8), WHILE PERFORMING A DVI INSPECTION ON THE L INBD FLAP, THE INSPECTION REVEALED THAT THE FWD PICK-UP FITTING INBD LOG AT RIB 5 WAS BROKEN IN HALF. THE FITTING LOT NR IS P4110. THE BROKEN OFF PIECE WAS FOUNSDR CA080912004Hinge Bracket · damaged(CAN) DURING THE REPLACEMENT OF THE REAR SPAR LT BRACKET, THE LT OTBD FLAP WAS REMOVED FOR ACCESS AND FOUND THE INBD HINGE OTBD BRACKET WITH DAMAGE CAUSED BY THE ROLLER BEARING FLANGE APROX 0.025 DEEP. DECIDED TO PERFORM DVI OF ALL REMAINING FLAP ROLLER ASSY SDR SWAA085028Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR DHLA2008745574Rib · crackedRT WING OTBD MID FLAP LOWER AFT SECTION AT WBL 492 RIB CRACKED. REPLACED RIB AT RT WING OTBD MID FLAP IAW B727 SRM 51-10-1 PARA 7.SDR DHLA2008745557Support Fitting · crackedLT WING INBD MID FLAP WBL 129.2 RIB SUPPORT FITTING CRACKED AT FWD LOWER SECTION. REPLACED LT WING INBD MID FLAP SUPPORT FITTING AT FWD LOWER SECTION WBL 129.2 IAW B727 SRM 51-10-1 PARA 7A.SDR ASAA0843601Skin · chafedRIGHT O/B MID FLAP LOWER SURFACED CHAFED BELOW NR 7 FLAP CARRIAGE. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS IAW B737 400 SRM 51 70 10 PG 214 AND BONDED IAW B737 400 SRM 51 70 10 PG 254.SDR ASAA0843598Skin · dentedRT AFT FLAP LOWER SURFACE DENTED WITHIN EDGE BAND. REMOVED, DAMAGED SKIN, FABRICATED FILLER AND DOUBLER, BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA0843577Skin · dentedLEFT WING I/B AFT FLAP UPPER SURFACE AREAS OF DENTS. PREPARED DAMAGED AREA, FABRICATED DOUBLERS, TREATED, REPAIRED AND BONDED IAW SRM 51-70-10 REPAIR 2.SDR ASAA0843571Skin · wornLEFT WING INBOARD AFT FLAP EXHAUST GATE WORN ON UPPER SURFACE. REMOVED DAMAGED UPPER PANEL, LOCATED, DRILLED AND INSTALLED A REPLACEMENT UPPER PANEL IAW B737 400 SRM 51 40 02 51 40 05.SDR SWAA085003Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR SWAA084999Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR SWAA084998Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM.SDR SWAA084992Skin · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP INBOARD END DELAMINATED. REPAIRED FLAP PER SRM.SDR 08FDEA03816Skin · dentedRT WING INBD FLAP FOUND DEEP DENT ON LOWER SKIN 0.25 INCH BY 0.25 INCH DEEP .074 INCH (SUSPECT CRACK ). REPAIRED DENT IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR UPS08153309Fairing · dentedINSPECTION TYPE:N/A, NR 4 MOVEABLE FLAP FAIRING DENTED OUT OF LIMTS. DETERMINED DAMAGE TO BE THREE DENTS. DENTS MEASURE AS FOLLOWS: DENT FWD IS 1.3" X 1.0, CENTER DENT IS 2.2" X 1.6" & AFT DENT IS .6" X 1.4". INSPECTED AND TAPED DENTS PER EO A300-5720-3052SDR 08FDEA03785Skin · dentedRT WING INBOARD FLAP LOWER SKIN CENTER AREA FOUND WITH SEVERAL DENTS. TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR SWAA084917Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR USAA920081654Wedge · delaminatedCLT C4 MAJOR REPAIR NR 03C30057003/017 & LOG NR 5030687. 2 AREAS OF DELAMINATION ON LT OTBD FOREFLAP WEDGE UPPER SURFACE. REPLACED LT OTBD FOREFLAP IAW B737 AMM 27-51-37.SDR USAA920081646Flap · delaminatedCLT Q1 MAJOR REPAIR NR 03C40727023/010 & NR 5030682. RT OTBD AFT FLAP DELAMINATED UPPER & LOWER SURFACE OF INBD END CAP. REPLACED RT OTBD AFT FLAP IAW B737 SRM 51-70-10.SDR DHLA2008745606Skin · corrodedRT WING I/B MID FLAP L/E INNER SKIN WITH CORROSION AT WBL 136. REPAIRED RT WING INBOARD MID FLAP LEADING EDGE SKIN SECTION FROM WBL 134 TO WBL 140 IAW COOPESA EO COO-2-57-321-08 DTD 09/29/08.SDR DHLA2008745559Strap · corrodedLT WING INBD MID FLAP INBD SECTION STRAP WITH CORROSION AT WBL 132. REPLACED LT WING INBD MID FLAP I/B SECTION STRAP IAW B727SRM 51-10-1 PARA 7A.SDR DHLA2008745558Strap · corrodedRT WING INBD MID FLAP INBD SECTION STRAP WITH CORROSION AT WBL 116. REPLACED STRAP IAW SRM 51-10-1 PARA 7A.SDR DHLA2008745542Angle · crackedLT WING I/B MID FLAP T/E I/B SECTON AFT LOWER CHORD ANGLE CRACKED AT WBL 125.SDR DHLA2008745541Strap · corrodedRT WING I/B MID FLAP L/E INNER SECTION STRAP WITH CORROSION FROM WBL 127 TO 143.SDR AALA200802276Wedge · delaminatedAFW RT OTBD FLAP TRAILING EDGE WEDGE ON TOP SIDE HAS DELAMINATION CUT OUT WITHIN 3.5 INCHES OF THE LEADING EDGE. AREA OF DISCREPANCY IS 12 INCH BY 6 INCH. REPAIRED PER SRM 57-53-01-2R TABLE 201.SDR 08FDEA03728Skin · damagedLT WING O/B FORE FLAP I/B SEQUENCE CARRIAGE HAS ELONGATED BOLT HOLES AT AFT END WBL 348 REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLESDR ASAA0843446Skin · dentedRIGHT I/B FOREFLAP LOWER SURFACE ABOVE NR 3 TIRE IS DENTED ON A REPAIR DOUBLER. REPAIRED THE DAMAGED AREA OF THE LOWER SURFACE OF I/B FORE FLAP IAW B737 400 SRM 51-70-10 REPAIR 4.SDR 2008FA0000639Hinge · corrodedFLAP HINGES IN ALL POSITIONS BOTH LT AND RT HAVE INTERGRANDULAR CORROSION NEAR THE POINT OF FAILURE. PN 13431-003, PN 13431-004, 13432-002, QTY 2, 13433-006, 13433-005. CONDITION WAS FOUND AT ANNUAL INSPECTION. (K)SDR ASAA0843445Skin · dentedLT WING NR 3 SPOILER UPPER SURFACE HAS 2 EA INVERTED DENTS. REPAIRED NR 3 SPOILER UPPER SURFACE IAW B737 400 SRM 51-70-10 REPAIR 4.SDR ASAA0843444Skin · dentedLT WING I/B UPPER TRAILING EDGE PANEL HAS A SMALL DENT 85 INCHES O/B OF I/B END 9 INCHES FWD OF TRAILING EDGE. REPAIRED LT WING I/B UPPER TRAILING EDGE PANEL IAW B737 400 SRM 51-70-10 REPAIR.SDR ASAA0843443Skin · dentedLT WING I/B UPPER TRAILING EDGE PANEL DELAMINATED 2 EA PLACES AS MARKED 53 AND 70 INCHES O/B OF I/B END. REPAIRED LT WING I/B UPPER TRAILING EDGE PNL IAW B737 400 SRM 51 70 10 REPAIR 2 PG 201.
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