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 SWAA064400Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR DL757060941Support Fitting · wornTHE SUPPORT FITTING BORE OF THE OUTBOARD FLAP TRACK WAS FOUND WORN AND ELONGATED. THE BORE WAS REAMED TO A TRUE DIAMETER AND A BEARING WAS INSTALLED PER BOEING INSTRUCTIONS AS CONTAINED IN 455361-14.SDR QXEA200603098Vane · damagedC3 YYC - LEFT OUTER FLAP VANE, CENTER LEADING EDGE HAS A CHERRY MARK RIVET WITH A BROKEN HEAD. REPAIRED IAW SRM 51-25-16, 51-42-13.SDR DHL2006780119Skin · delaminatedLEFT WING I/B MID FLAP IS DELAMINATED AT TE LOWER SURFACE. REMOVED DELAMINATED AREA APPROX 7" BY 4.2". FAB FILLER APPROX 7" BY 4.2", FILLERS (2EA) 3" BY 4.2" AND STRAP 1" BY 4.4" FROM 7075T6 .016 PO NR 526029, ALODINED AND PRIMED REPAIR PARTS AND AREA TO BE SDR DHL2006807511Frame · crackedLT INBD FLAP FORMER 1" CRACK STA XW 122.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10 (AL2024T3 0.063"). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER IAW SRM 57-2SDR DHL2006780114Skin · delaminatedLEFT WING, INBD FORE FLAP, UPPER SURFACE, INBD SIDE DELAMINATED. CUTOUT DELAMINATED SKIN AND HONEYCOMB CORE APPROX 2.5 BY 8. FABRICATED FILLER APPROX 2.5" BY 8" AND DOUBLER APPROX 4 BY 9.5 FROM P/N 2024-T3, .016, PO NR 9003189 AND HONEYCOMB P/N 3.1 3/16 5052SDR SWAA064376Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR 06FDEA03978Skin · damagedRT WING INB FLAP L/E EXISTING REPAIR AT STA XIFH240. EXISTING REPAIR REMOVED IAW SRM 57-30-00 VOL 2. FOUND RIB DISTORTED AND ILLEGAL REPAIR. REMOVED O/B SKIN AND CUT OUT SECTION. REMOVED 3 RIBS AND EXISTING ANGLE REPAIR IAW SRM 51-30-00 VOL 2. RIB P/N F17SDR SWAA064337Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.SDR DHL2006807507Skin · wornRT OTBD FLAP UPPER SKIN WORN STA XF 349.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.063") IAW SRM 57-7-1 FIG 4 ITEM "BSDR SWAA064325Skin · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED ON INBOARD T/E. REPAIRED FLAP PER SRM.SDR SWAA064324Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.SDR DLM88070411Skin · delaminatedREPAIR OF RT INBD FLAP/INBD VANE - TWO AREAS OF DELAMINATION ON THE L/E SKIN AND ONE ON THE LOWER SURFACE BETWEEN STAXIVIF=6.2364 AND XIVIF=35.5571. PERMANENT REPAIRS INSTALLED PER AEROMEXICO REPAIR DRAWING NR AMR0957141 R03 DATED 24AUG06 VIEW C AND REPAIR SKSDR 2006UALA02162Hinge Fitting · crackedRT WING INBD FLAP AFT CENTER HINGE FITTING OUTBD FLANGE IS CRACKED. FABRICATED REPAIR PARTS PER SRM 57-53-02 AND INSTALLED FITTING PER SRM 51-40-4 ON NON ROUTINE W1762V. INSPECTED AND OK'ED FOR RETURN TO SERVICE.SDR 2006UALA02161Hinge Fitting · crackedLT WING INBD FLAP, AFT CENTER HINGE FITTING OUTBD FLANGE IS CRACKED. LT WING INBD FLAP, AFT CENTER HINGE FITTING OUTBD FLANGE IS CRACKED. FABRICATED FITTING REPAIR PARTS PER SRM 57-53-02 AND INSTALLED PER SRM 51-40-04 ON NON ROUTINE T2145Y. INSPECTED AND OKSDR ASAA0641191Wedge · chafedRIGHT I/B MID FLAP T/E WEDGE IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51-70-10.SDR ASAA0641187Skin · damagedLT IB FORE FLAP HAS NUMEROUS DINGS BELOW CENTERLINE TRACK. PREPPED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10 REPAIR 2.SDR ASAA0641184Skin · chafedLT OB MID FLAP PREVIOUS REPAIR AT NR 2 FLAP TRACK IS CHAFED. REMOVED DAMAGED DOUBLER. FABRICATED AND INSTALLED REPAIR DOUBLER IAR SRM 51 70 10.SDR ASAA0641183Skin · dentedRT IB FORE FLAP LWR SKIN DENTED. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.SDR ASAA0641182Skin · dentedRT IB TE FLAP LWR SKIN HAS MULTIPLE DENTS. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10 REPAIR 2.SDR DLM88070415Skin · damagedLT WING INBD FLAP LOWER SKIN P/N 9935942-5 REPAIR - EXISTING REPAIR FOUND ON L/H WING INBD FLAP LOWER SKIN PANEL. DATA SENT TO BOEING FOR APPROVAL. BOEING REQUESTED INSTALLATION OF ADDITIONAL REPAIR SPLICE ON INTERNAL REB AT STA XIFO=110.608. REPAIR SPLICE SDR UPS07M48872Hinge · corrodedINSPECTION TYPE:C LT WING, I/B FLAP O/B HINGE (FLAP SIDE) O/B LUG O/B FLANGE CORRODED. LHW IB FLAP OB HINGE AFT SIDE OB STRAP OB SURF LOCAL BLEND CORROSION REMAINING THK 0.205" AND CORROSION STILL EXIST MIN ALLOW THK 0.205" CMM57-52-03. ST ARP REMOVED SRM 51SDR UPS07M48871Hinge · corrodedINSPECTION TYPE:C RT WING, I/B FLAP O/B HINGE, O/B LUG O/B FLANGE CORRODED. RHW IB FLAP OB HINGE AFT SIDE OB STRAP OB SURF LOCAL BLEND CORRODED, REMAINING THK 0.205" AND CORROSION STILL EXIST MIN ALLOW THK 0.205" CMM 57-52-03. STRAP REMOVED SRM 51-33-01VISDR AWXA200601948Panel · delaminatedMCN - DELAMINATION ON RT WING TRAILING EDGE FLAP INBOARD PANEL NR 7420 TOP SURFACE 26" FROM OUTBOARD END. REPAIRED DELAMINATED AREA ON RT WING TRAILING EDGE FLAP INBOARD PANEL NR 7420 TOP SURFACE 26" FROM OUTBOARD END IAW B737-300 SRM 51-70-10-2R4, FIG 202 RESDR 06FDEA03915Support Fitting · crackedLT O/B FLAP I/B HINGE FWD SUPPORT FITTING CRACKED AT FWD NOSE SECTION REMOVED FASTENERS FOR NDT ACCESS. PERFORMED HFEC INSPECTION ON FWD HINGE SUPPORT FITTING I/B AND O/B HALVES FROM FWD END TO PERIPHERY AND IMMEDIATE AREAS OF THE FIRST THREE FASTENERS (3EA).SDR DLM88070414Skin · damagedRT INBD FLAP, REMOVABLE SECTION, LOWER SKIN REPAIR - TWO TEMP REPAIRS FOUND ON FLAP PANEL P/N 9935942-6. PERMANENT REPAIRS INSTALLED PER AM REPAIR DRAWING AMR0957173 R01 AND ERA 457448-14.SDR USAA061330Skin · damagedRIGHT OUTBOARD AFT FLAP LEADING EDGE, BETWEEN INBOARD TRACK AND SECOND TRACK NEEDS REPAIR. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 4, DEFECT SIZE: 88 X 8.5 INCHES.SDR USAA061329Skin · damagedRIGHT OUTBOARD FORE FLAP LEADING EDGE AT OUTBOARD END NEEDS REPAIR. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 1, DEFECT SIZE: 6 X 4.5 INCHES.SDR USAA061325Skin · delaminatedLEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.SDR ASAA0681178Skin · puncturedLEFT WING INBOARD FLAP VANE IS PUNCTURED. REPLACED DAMAGED SKIN SECTION AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 57 03.SDR S9BA00906Hinge · corrodedDURING INSPECTION, FOUND LT IB FORE FLAP IB HINGE (PN 6WFM1109-33) WITH ATTACHED RIB CORRODED.SDR S9BA00806Hinge · corrodedDURING INSPECTION, FOUND LT IB FORE FLAP OB HINGE (PN C6WF1101045) CORRODED.SDR DHL2006780110Skin · delaminatedRT WING, INBD AFT FLAP T/E LWR SURFACE, WBL 124.0, WS 251. VARIOUS DENTS INBD AND OUTBD OF NR 5 FLAP TRACK. INSPECTION FOUND DELAMINATION BETWEEN DENTS. REMOVED DELAMINATED AREA. CUTOUT 13.5 BY 14.75 CLEANED, PREPPED AREA TO BE REPAIRED IAW B727 SRM PARA 6 SDR DHL2006780108Skin · delaminatedRT WING, AFT FORE FLAP UPPER SURFACE, OUTBD T/E HAS AREA DELAMINATING WBL249. CUTOUT DELAMINATED AREA ON RT INBD FORE FLAP OUTBD T/E, UPPER SURFACE APPROX DIM 4" BY 15.1". FAB FILLER APPROX 1" BY 15.1" AND DOUBLER APPROX 4 BY 15.1", 7075-T6, PO NR 5397662. SDR 06FDEA03865Skin · misrepairedSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. BY: 067708 (N252) PREVIOUS COMPOSITE REPAIR FOUND LOCATED ON RT INB FLAP, UPPER SURFACE OUTB END, FLAP RIB 19. REPAIR REQUIRES EVALUATION SDR DHL2006780109Skin · delaminatedRT WING, OUTBD FORE FLAP LWR SURFACE, OUTBD FITTING, DELAMINATION JUST BELOW FITTING, WBL 395, WS 550. CUTOUT DELAMINATED AREA ON RT OUTBD FORE FLAP APPROX DIM 1" BY 1". FAB FILLER APPROX 1" BY 1" AND DOUBLER APPROX 2.25 BY 4 FROM 2024-T3, 0.016, PO NR 90031SDR DLM88060923Skin · delaminatedDURING VISIT, TWO AREAS OF DELAMINATION WERE FOUND IN THE SKIN LOWER SURFACE. AREAS REPAIRED PER BOEING INSTRUCTIONS, SEE ERA 457446-14SDR QXEA200602979Skin · gougedC1 OKC - LEFT OUTBOARD FLAP HAS GOUGE DAMAGE ON LEADING EDGE, INBOARD CORNER. REPAIRED IAW SRM 51-42-06 AND 51-42-20, 51-42-10.SDR QXEA200602973Support · wornC1 OKC - RIGHT WING OUTBOARD FLAP VANE SUPPORTS ARE WORN EXCESSIVELY AND HAVE DISPLACED METAL. REPAIRED IAW SRM 51-12-00.SDR SWAA064219Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT OUTBOARD AFT T/E FLAP LOWER INBOARD SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR 06FDEA03860Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL DIA: 1.240", FINAL DIA: 1.283", MAX ALLOWABLE DIA: 1.220". BUSHING FABRICATED AND INSDR 06FDEA03859Hinge · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE), LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-408 AND FOUND WITHIN DAC ARC0503 LIMITS. ORIGINAL THK I/B: 0.474", O/B: 0.469", REMAINING THK I/B: 0.472", O/B: 0.467", MATERISDR 06FDEA03858Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG 621-622. ORIGINAL DIA: 1.148", FINAL DIA: 1.152", MAX ALLOWABLE DIA: 1.150". BUSHING FABRACATED AND INSDR DHL2006780106Skin · delaminatedLEFT WING AFT FLAP UPPER SURFACE, INBD END DELAMINATED. CUTOUT DAMAGE/DELAMINATED AREA APPROX DIM 3" BY 1". FAB FILLER APPROX 3" BY 1" AND DOUBLER APPROX 6 BY 2.5" FROM P/N 7075-T6, .012, PO# 5397662. CLEANED, ANODIZED, PREPPED AND PRIMED AREA, FILLER AND DSDR DHL2006780102Skin · damagedTIRE DEBRIS DAMAGE ON LEFT WING INBD AFT FLAP LWR SURFACE. CUTOUT DAMAGE/DELAMINATED AREA ON LT INBD AFT FLAP LWR SURFACE APPROX DIM 13" BY 15". FAB FILLER APPROX 13" BY 15" AND DOUBLER APPROX 15" BY 16" FROM P/N 2024-T3, .016, PO NR 9003189. CLEANED, PREPPSDR DHL2006780006Skin · delaminatedLEFT WING AFT FLAP UPPER SURFACE, INBD END DELAMINATED. CUTOUT DAMAGE/DELAMINATED AREA APPROX DIM 3" BY 1". FAB FILLER APPROX 3" BY 1" AND DOUBLER APPROX 6 BY 2.5" FROM P/N 7075-T6, .012, PO NR 5397662. CLEANED, ANODIZED, PREPPED AND PRIMED AREA, FILLER ANDSDR AWXA200601947Structure · debondedMCN - DEBOND AREA AT TRAILING EDGE OF RT INBOARD FOREFLAP, 4.5" FROM OUTBOARD END. REPLACED DEBOND AREA AT TRAILING EDGE OF RT INBOARD FOREFLAP 4.5" FROM OUTBOARD END IAW B737 SRM 51-70-10-2R, REPAIR 4, FIG 203.SDR USAA061303Skin · delaminatedLEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.SDR PIDR2006039Skin · delaminatedDELAMINATION AT THE IB END OF THE LT OB FORE FLAP. REPAIRED DAMAGED AREA IAW SRM 51-70-10.SDR SWAA064171Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD LOWER L/E. REMOVED AND REPLACED AFT FLAP PER MM.
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