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 06FDEA04281Hinge Bracket · corrodedRHW I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-106574 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04280Hinge Bracket · corrodedRHW O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG. 621-622. ORIGINAL THK 1.151" FINAL 1.151" MAX. ALLOWABLE THK 1.150". BUSHING FABRICATED AND INSTALLEDSDR 06FDEA04279Hinge Bracket · corrodedRHW I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. RT AFT I/B FLAP O/B HINGE PIVOT I/B BORE CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL THK 1.2555" FINAL 1.2555" MAXIMIUM ALLOWABLESDR 06FDEA04278Hinge Bracket · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL 1.2555" FINAL 1.2555" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PSDR 06FDEA04269Hinge · corrodedRIGHT WING, WINGSIDE OUTBD FLAP INBD HINGE NR 7 LOWER MOUNT SURFACE FOUND CORROSION. REWORKED AND REPAIRED PER EA 1-5750-105576 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR ASAA0641327Skin · chafedRIGHT OUTBOARD MID FLAP INBOARD SIDE LWR SURFACE OF L/E HAS CHAFING DAMAGE. REPAIRED OUTBOARD MID FLAP L/E IAW SRM 57-53-01 FIG 201.SDR QXEA200603183Flap Track · corrodedC4 PDX - RIGHT WING NR 5 FLAP TRACK HAS CORROSION ON FORWARD ATTACH POINT BETWEEN SPIGOT PLATE AND UPPER SURFACE OF FLAP TRACK. REPAIRED IAW AMM 57-50-51-000-801, 57-50-51-400-802, AND 57-50-51-400-801.SDR L43A12170601Spar · corrodedA/C IS IN "C" CHECK, VISUAL INSPECTION POINTED TO POSSIBLE CORROSION IN RT INB MAIN FLAP. AFTER DISASSEMBLY OF FLAP THE AFT SPAR CHORD WAS FOUND TO HAVE CORROSION IN NUMEROUS PLACES. A REPLACEMENT MAIN FLAP HAS BEEN PURCHASED FOR INSTALLATION. DISCREPANCY ESDR UIEA2006306Skin Panel · damagedLT WING OUTBOARD MID-FLAP L/E DAMAGE AT OUTBOARD TRACK CUT-OUT. PERMANENT COMPOSITE REPAIR TO L/E WAS ACCOMPLISHED AS PER B747 SRM 51-40-14 AND PERMANENT REPAIR TO RIB SECTION LOCATED AT WBL 794, AS PER B747 SRM 51-40-03 FIG 1. ALSO, REFERENCE ATLAS AIR EO 4SDR ASAA0641329Skin · debondedRIGHT O/B AFT FLAP I/B END DISBONDING. RIGHT O/B AFT FLAP I/B END REPAIRED IAW EA 57 50 02309.SDR USAA061438Skin · chafedINBOARD FOREFLAP, TRAILING EDGE, BOTTOM SIDE, 12 INCHES OUTBOARD OF AFT FLAP CUTOUT CHAFED. CUT OUT DAMAGE, HONEYCOMB REPAIR WITH DOUBLERS PER SRM 51-70-10, DEFECT SIZE: 1 INCH.SDR QXEA200603346Flap Track · corrodedPDX C4 LEFT WING INBOARD FLAP INBOARD LOWER TRACK HAS PITTING ON UPPER SURFACE AT APPROXIMATELY 20" FROM FORWARD EDGE. REPAIRED IAW RD 8-57-985.SDR AWXA200700034Skin · delaminatedMCN - RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED, WBL 119 - WBL 121. REPAIRED RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED, WBL 119 - WBL 121 IAW B737-300 SRM 51-70-10-2R3, FIGURE 201.SDR 06FDEA04244Hinge · corrodedLEFT WING I/B FLAP O/B HINGE NR 1 I/B PIVOT HOLE FOUND CORROSION. REPAIR CARRIED OUT AT LEFT WING (FLAP) I/B FLAP O/B HINGE NR 1 I/B PIVOT HOLE AS PER FEDEX EA 1-5750-105578. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR SWAA064951Arm · corrodedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD CARRIAGE INBOARD ARM CORRODED. REMOVED AND REPLACED CARRIAGE ARM PER MM.SDR SWAA064950Arm · corrodedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD CARRIAGE OUTBOARD ARM CORRODED. REMOVED AND REPLACED CARRIAGE ARM PER MM.SDR DL76G070543Fitting · crackedLT IB FLAP AFT FLAP I/B FITTING CRACKED AT ATTACHING FASTENERS. REPAIRED PER SRM 57-53-02 FIG 201.SDR AWXA200700029Skin Panel · delaminatedSAL - RIGHT WING OUTBOARD FLAP UPPER AND LOWER SURFACES DELAMINATED, WS 5512, RIB 10. REPAIRED RIGHT WING OUTBOARD FLAP UPPER AND LOWER SURFACES DELAMINATED, WS 5512, RIB 10 IAW A320 SRM 57-53-00 FIGURE 212.SDR 06FDEA04214Structure · corrodedLT WING (FLAP) I/B FLAP O/B HINGE NR 1 O/B PIVOT HOLE SURFACE FOUND CORROSION. REPAIR CARRIED OUT AT LEFT WING (FLAP) I/B FLAP O/B HINGE NR 1 O/B PIVOT HOLE AS PER FEDEX EA 1-5750-105578. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA04213Structure · corrodedLT WING (FLAP) I/B FLAP O/B HINGE NR 1 I/B PIVOT HOLE SURFACE FOUND CORROSION. REWORKED AND REPAIR CARRIED OUT AT LEFT WING (FLAP) I/B FLAP O/B HINGE NR 1 I/B PIVOT HOLE SURFACE AS PER CMM 57-52-03. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR USAA061404Skin · crackedA 49 INCHES FROM I/B END OF RIGHT O/B AFT FLAP. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: .25 INCH.SDR ASAA0641314Skin · delaminatedLT OB AFT FLAP IB END IS DELAMINATED. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51 70 10 PG 249.SDR ASAA0641313Skin · delaminatedLT OB FORE FLAP DELAMINATED AT IB EDGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 51 70 10 PG 244.SDR QXEA200603323Skin · dentedYYC C3 - LEFT INBOARD FLAP AREA BETWEEN INBOARD END AND STATION 38.00 HAS SEVERAL DENTS IN SKIN. REPAIRED IAW CRJ700 SRM 57-52-01-001-001-A01 AND 51-12-00-001-001-A01.SDR 06FDEA04199Skin · gougedPREVIOUSLY INSTALLED REPAIR ON LT OTBD FORE FLAP 10" FROM INBD END HAS GOUGE ON DOUBLER REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 57-50-4 FIG PG 1. THIS REPAIR CLASSIFIED AS MAJOR ON WO NR 34610, SNRM NR N01238.SDR QXEA200603281Skin · chafedC3 OKC - RIGHT WING OUTBOARD FLAP INBOARD GUIDE IS CHAFED. REPAIRED IAW REO670-57-51-036.SDR QXEA200603266Fitting · damagedC3 OKC - LEFT WING OUTBOARD FLAP BOTH MID FLAP AND VANE FITTINGS HAVE HIGH METAL. REPAIRED IAW SRM 57-53-01 AND 51-12-00.SDR QXEA200603265Fitting · gougedC3 OKC - LEFT WING INBOARD FLAP GUIDE FITTING IS GOUGED. REPAIRED IAW REO670-57-51-036.SDR AWXA200602093Skin · delaminatedMCN - LEFT WING OUTBOARD FORE FLAP UPPER SKIN DELAMINATED, WBL 203.69. REPAIRED LEFT WING OUTBOARD FORE FLAP UPPER SKIN, WBL 203.69 IAW B737-300 SRM 51-70-10.SDR SWAA064799Flap · debondedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.SDR QXEA200603267Panel · chafedC3 OKC - LEFT INBOARD FLAP PANEL 584DB CHAFED. REPAIRED IAW SRM 51-12-00 AND 57-41-01, 51-21-16.SDR QXEA200603274Panel · tool damageC3 OKC - LEFT WING FLAP PANEL 584CB TOOL MARK AT ATTACHMENT HOLE. REPAIRED IAW SRM 51-12-00, 57-41-01, AND 51-21-16.SDR QXEA200603273Panel · chafedC3 OKC - LEFT WING FLAP PANEL 584AB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 57-41-01, AND 51-21-16.SDR QXEA200603272Panel · chafedC3 OKC - LEFT WING FLAP PANEL 584GB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 57-41-01, AND 51-21-16.SDR QXEA200603271Panel · chafedC3 OKC - LEFT WING FLAP PANEL 584EB CHAFED AT CUTOUT. REPAIED IAW SRM 51-12-00, 57-41-01, AND 51-21-16.SDR QXEA200603270Panel · chafedC3 OKC - LEFT WING FLAP PANEL 584JB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 57-41-01, AND 51-21-16.SDR QXEA200603269Panel · chafedC3 OKC - LEFT WING FLAP PANEL 584LB CHAFED AT CUTOUT. REPAIRED IAW SRM 51-12-00, 57-41-01, AND 51-21-16.SDR SWAA064725Skin · debondedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DISBONDED. REPAIRED FORE FLAP PER SRM.SDR SWAA064724Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP INBOARD FWD CORNER DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA064690Flap · delaminatedDURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED AFT FLAP PER MM.SDR DLM88061028Skin · gougedTHE LT INBOARD FLAP, OUTBOARD TE WEDGE LOWER SKIN IS GOUGED AT STATION W 59.450. THE DAMAGED SKIN WAS CUT OUT AND NEW SECTION OF SKIN WAS SPLICED IN.SDR DHL2006741004Skin · delaminatedRT WING OUTBD AFT FLAP TE HAS DELAMINATE SPOT AT WBL 445 APPROX (MARKED). CUT OUT DELAMINATED AREA APPROX 4" BY 2". FABRICATED FILLER APPROX 4"BY 2" AND DOUBLER APPROX 7" BY 3 1/2", MAT ID 7075T6 .016 PO NR 526029. PREPARED DAMAGED SURFACE, FILLER AND DOUBLSDR NOCA20906Bracket · crackedBRACKET CRACKED ON RIGHT WING O/B FLAP I/B END CAP NEAR DATA PLATE. REMOVED AND REPLACED CRACKED BRACKET ON RIGHT WING I/B END OF O/B FLAP.SDR SWAA064637Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED INBOARD AFT FLAP PER MM.SDR SWAA064631Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FOREFLAP PER MM.SDR 06FDEA04143Fitting · damagedLT WING I/B FLAP I/B ENCLOSURE AFT UPPER BIG ROLLER BEARING ATTACHMENT FITTING FOUND HOLE ELONGATED AS MARKED. REPAIRED AS PER EA 1-5750-106545. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.SDR AMTA200600687Skin · damagedLT IB FLAP HAS DAMAGE TO BULLNOSE AND LWR SURFACE PANEL AND 2 EA ENCERNTRIC BUSHINGS, ITEMS REMOVED FROM ONE AC TO THIS AC AND NEED TO BE REPAIRED IAW COMPANY. REPAIRED IAW EA, SRM. (K)SDR SWAA064619Gimbal Joint · corrodedDURING SCHEDULED 20Y CHECK, FOUND LEFT WING INBOARD FLAP INBOARD GIMBAL ASSY CORRODED. REMOVED AND REPLACED GIMBAL ASSY PER MM.SDR USAA200611001Wedge · delaminatedA 3 X 12 INCH AREA OF CORE DAMAGE/DELAMINATION AT RIGHT I/B MID FLAP T/E WEDGE. REMOVED DAMAGED WEDGE AND INSTALLED NEW WEDGE PER BOEING DWG 113N2003.SDR DHL2006807526Skin · delaminatedNR 5 LT VANE FLAP LWR SKIN DELAMINATED 8". REMOVED AND REPLACED NR 5 LT VANE FLAP IAW MM 27-51-14 PG 201-202. REFER TO NR 070100 FOR OPS CHECK.
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