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 AWXA200601583Skin · debondedMCN - DISBOND AREA ON UPPER SURFACE OF LT O/B FOREFLAP 119", FROM I/B END. REPAIRED DISBONDED AREA ON UPPER SURFACE OF LT O/B FOREFLAP 119" FROM I/B END, IAW B737-300 SRM 51-70-10-2R, REPAIR 4, FIG 201.SDR AWXA200601582Skin · debondedMCN - DISBOND AREA ON UPPER SURFACE OF LT O/B FOREFLAP 6" FROM I/B END. REPAIRED DISBONDED AREA ON UPPER SURFACE OF LT O/B FOREFLAP 6" FROM I/B END IAW B737-300, SRM 51-70-10-2R REPAIR NR 4, FIG 202.SDR AWXA200601574Skin · debondedMCN - DISBOND AREA ON LOWER SURFACE OF RT OUTBOARD FOREFLAP, AT TRAILING EDGE, 18.5" FROM INBOARD END. REPAIRED DISBOND AREA ON LOWER SURFACE OF RT OUTBOARD FOREFLAP AT TRAILING EDGE, 18.5" FROM INBOARD END IAW B737-300 SRM 51-70-10-2R4, FIG 202.SDR AWXA200601573Skin · debondedMCN - DISBOND AREA ON UPPER SURFACE OF RT INBOARD FOREFLAP, 36.5" FROM OUTBOARD END, 9" FROM AFT EDGE. REPAIRED DISBOND AREA ON UPPER SURFACE OF RT INBOARD FOREFLAP 36.5" FROM OUTBOARD END, 9" FROM AFT EDGE, IAW B737-300 SRM 51-70-10-2R4, REPAIR 4, FIG 201.SDR SWAA063242Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD LOWER END. REMOVED AND REPLACED AFT FLAP PER MM.SDR AWXA200601572Skin · debondedMCN - DISBOND AREA ON LOWER SURFACE OF RT OUTBOARD FOREFLAP, NEAR OUTBOARD END. REPAIRED LOWER SURFACE OF RT OUTBOARD FOREFLAP NEAR OUTBOARD END, IAW B737-300 SRM 51-70-10-2R4 (REPAIR 4) FIG 202.SDR USAA061074Skin · chafedFOUND CHAFED AREA RIGHT OUTBOARD MID FLAP AT INBOARD END OF LEADING EDGE. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 8 DEFECT SIZE: 4" BY .4" BY .025".SDR 06FDEA03115Skin · dentedRT WING I/B FLAP LOWER SURFACE FOUND DENT. REPAIR CARRIED OUT AT RH WING I/B FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR DHL2006781001Structure · chafedLEFT WING O/B FOREFLAP CHAFING ON LWR LEADING EDGE AT O/B ATTACH POINT. BLENDED OUT AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 3. CUTOUT DAMAGED AREA (1/2" BY 5/8") IAW B727 SRM 57-50-4 FIG 1. FAB REPAIR DOUBLER (5"X4") FROM 2024-0 .050 PO NR 9SDR SWAA063180Flap · vibratesDURING FLAPS EXTENSION TO POSITION 5, A STEADY VIBRATION FELT IN BOTH CONTROL COLUMNS. REMOVED AND REPLACED LT WING INBOARD FORE FLAP PER MM.SDR DHL2006782Flap · delaminatedLEFT WING T/E FLAP ASSEMBLY T/E SEGMENT HAS TWO AREAS OF DELAMINATION BETWEEN THE FLAP TRACKS AND ONE AREA AT INBOARD END WHERE A PREVIOUS REPAIR IS LIFTING AND OPENED UP.SDR AWXA200601541Structure · delaminatedMCN - LT WING I/B MAIN FLAP HAS A DISBONDED AREA AT THE O/B T/E CORNER. REPAIRED LT WING, I/B MAIN FLAP O/B T/E CORNER, IAW B757-200, SRM 51-70-10-2R, FIG 201.SDR SWAA063157Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT WBL 150. REMOVED AND REPLACED FORE FLAP PER MM.SDR QXEA200602380Skin · chafedPDX - C3 CHECK - LEFT FLAP INBOARD VANE CHAFED ON LEADING EDGE ABOVE INBOARD ACTUATOR. SMOOTHED CHAFE IAW SRM 51-12-00 MATERIAL LOSS .002". WITHIN LIMITS PER SRM. PRIMED AND PAINTED AREA.SDR 06FDEA03054Skin · damagedFOUND REPAIR LOCATED RT OUTBD FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO ANSDR 06FDEA03049Skin · damagedFOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR COVERED BY RAS REF : RAS /DA/BRE/1642/97, REPAIR EVALUATESDR 06FDEA03048Skin · damagedFOUND REPAIR LOCATED LT INB FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISSDR 06FDEA03047Skin · damagedFOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INDB OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRSDR 06FDEA03046Skin · damagedFOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX ENGINEERING AUTHORIZSDR UPS06847782Doubler · gougedINSPECTION TYPE:C1-3 STA 219 LT FLAP FOUND O/B VERT DOUBLER AND LWR ATTACH ANGLE GOUGED OUT OF LIMITS. REMOVED DAMAGED DOUBLER AND ATTACH ANGLE AT LT FLAP STA 219 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT REPAIR WEB, STRAP AND REPAIR ANGLE IAW DSDR USAA061052Skin · chafedRT WING OUTBD FLAP APPROX 4 FT O/B OF I/B FLAP TRACK CHAFED. CUT OUT DAMAGE, INSTALLED REPAIR PARTS, TREATED, PRIMED & TOP COATED PER SRM 57-53-01 & 51-40-02, DEFECT SIZE: 2.1" X 1.1", DEPTH .060".SDR SWAA063091Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA063082Toggle · wornVIBRATION REPORTED WITH FLAPS AT 5 AND 180 KNOT AIRSPEED. REMOVED AND REPLACED LT WING AFT FLAP TOGGLES PER MM.SDR 06FDEA03017Hinge Bracket · corrodedRT WING INBD FLAP (FLAP SIDE) OUTBD PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. RT AFT I/B FLAP O/B HINGE PIVOT I/B BORE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL THK 1.187" FINAL 1.259" MAX ALLOWABLE 1.220". BUSHISDR 06FDEA03015Skin · dentedRT WING INBD FLAP OUTBD SEGMENT LOWER SURFACE FOUND SEVERAL DENT MARKS. RT WING I/B FLAP O/B SEGMENT LOWER SKIN REMOVED AS PER SRM 51-33-01 AND SRM 51-35-01 VOL II. NEW SKIN FABRICATED USING MATERIAL 2024T3- 0.040" THK AS PER DWG NR ARC 2444, REPROTECTED ASDR 06FDEA03014Skin · dentedLT WING INBD FLAP INBD SEGMENT LOWER SKIN FOUND NUMEROUS DENT MARK. LT WING I/B FLAP I/B SEGMENT LOWER SKIN REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 2 VOL I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.SDR 06FDEA03013Skin · dentedRT WING INBD FLAP INBD SEGMENT LOWER SURFACE FOUND SEVERAL DENT MARKS. RT WING I/B FLAP I/B SEGMENT LOWER SKIN REPAIR CARRIED OUT AS PER SRM 57-00-00 FIG 2 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.SDR 06FDEA03012Skin · dentedLT WING INBD FLAP OUTBD SEGMENT LOWER SKIN FOUND NUMEROUS DENTS. LT WING I/B FLAP O/B SEGMENT LOWER SKIN REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 2 VOL I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.SDR 06FDEA03016Hinge Bracket · corrodedLT WING INBD FLAP (FLAP SIDE) OUTBD PIVOT PIN ATTACHMENT OUTBD STRAP SURFACE FOUND CORRODED. LT WING I/B FLAP O/B HINGE O/B STRAP PIVOT STRAP SURFACE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL THK 0.273" REMAINING TSDR 06FDEA3012Skin · dentedLT WING INBD FLAP OUTBD SEGMENT LOWER SKIN FOUND NUMEROUS DENT MARK AS MARKED.SDR 06FDEA3013Skin · dentedFOUND RT WING INBD FLAP INBD SEGMENT LOWER SURFACE FOUND SEVERAL DENT MARK AS MARKED.SDR 06FDEA3014Skin · dentedLT WING INBD FLAP INBD SEGMENT LOWER SKIN FOUND NUMEROUS DENT MARK AS MARKED.SDR 06FDEA3015Structure · dentedFOUND RT WING INBD FLAP OUTBD SEGMENT LOWER SURFACE FOUND SEVERAL DENT MARK.SDR 06FDEA3016Hinge Bracket · corrodedLT WING INBD FLAP (FLAP SIDE) OUTBD PIVOT PIN ATTACHMENT OUTBD STRAP SURFACE FOUND CORRODED.SDR 06FDEA3017Hinge Bracket · corrodedFOUND RT WING INBD FLAP (FLAP SIDE) OUTBD PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED.SDR 06FDEA3018Hinge Bracket · corrodedRT WING INBD FLAP (FLAP SIDE) OUTBD PIVOT PIN ATTACHMENT OUTBD BORE FOUND CORRODED (HINGE BRACKET P/N ARC2512-504).SDR DHL2006809523Vane · damagedRT INBD VANE SLOT HOLES ELONGATED STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-12-06, EO NR AST060701 DATED 07-07-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW EO NR AST060701. PERFORMED SDR SWAA063050Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0680898Skin · gougedLEFT INBOARD FLAP OUTBOARD VANE L/E GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0680897Skin · dentedRIGHTHAND OUTBOARD FLAP INBOARD VANE DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0680896Skin · dentedLEFTHAND INBOARD FLAP OUTBOARD VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-2.SDR ASAA0680895Skin · gougedLEFTHAND INBOARD FLAP OUTBOARD VANE IS GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0680894Skin · dentedRIGHTHAND OUTBOARD FLAP INBOARD VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0680893Skin · dentedRIGHTHAND OUTBOARD FLAP VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0680892Skin · gougedLEFTHAND OUTBOARD FLAP VANE L/E GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.SDR ASAA0680891Skin · dentedLEFTHAND INBOARD FLAP OUTBOARD VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-2.SDR SWAA063019Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.SDR AWXA200601512Skin · delaminatedMAJOR REPAIR - CHECK NR C-15. NR 5880187. LT IB T/E FLAP, OB UPPER AND LOWER SURFACE, WAS FOUND WITH DELAMINATION. REPAIRED UPPER AND LOWER SURFACE ON LT IB TRAILING EDGE FLAP OB END, IAW SRM 51-70-10-2R4, FIG 202.SDR AWXA200601503Wedge · debondedRIGHT WING O/B FOREFLAP, LOWER SURFACE HAS DISBONDED AREA 7.5" FROM I/B END. RIGHT WING O/B FOREFLAP, LOWER SURFACE DISBONDED AREA 7.5" FROM I/B END REPAIRED I/A/W B737-300 SRM 51-70-10-2R4, REPAIR NR 4, FIGURE 202.SDR UIEA200600206Skin · damagedN496MC AT PIK FOR MSG C-4 & A-4 CHECK. AS PER N/R 39, ON INDUCTION OF A/C FOUND LT I/B T/E FORE FLAP LEADING EDGE DAMAGED, I/B OF NR 3 CANOE. OFF S/N 000532. RECT:LT, I/B T/E FORE FLAP REPLACED AS PER AMM 27-51-02. ON P/N 65B39011-93C & ON S/N 000492.
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