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 FDEA201110144495Skin · misrepairedRT WING INBD FLAP UPPER SEGMENT LOWER SKIN MISREPAIRED. CARRIED OUT REPAIR AS PER EA 1-5750-154239 .SDR FDEA201110144503Skin · puncturedLEFT WING, INBD FLAP, LOWER OTBD SKIN PUNCTURED. TRIMMED OUT DAMAGE IAW 57-00-01, HFEC IAW NTSPM 06-10-01. NO CRACKS NOTED. FABRICATED SKIN DOUBLER, TEE DOUBLERS, TEE FILLER AND SKIN FILLER IAW SRM 57-00-01 FIG.3 INSTALLED ALL REPAIR PARTS IAW SRM 57-00-0SDR A6WA201141086Skin · chafedLT INBD FLAP VANE SKIN HAS CHAFING DAMAGE IN 3 EA FROM STOPS EVALUATED DAMAGE ON LT INBD FLAP VANE IAW SRM 51-12-00 BLENDED IAW SRM 51-12-00 MAT LOSS .019 AT FLAP STATION 60.005.015 AT FLAP STATION 98.505.005 AT FLAP STATION 137.012 WITHIN SERVICEABLE LIMITS ISDR USAA2011102700008Skin · delaminatedC1 CHECK - DELAMINATION ON RIGHT WING OUTBOARD FLAP BOTTON SKIN AT WS 821. REPAIRED RIGHT WING OUTBOARD FLAP BOTTOM SKIN AT WS 821 IAW SRM 51-70-17-0G FIGURE 10.SDR QXEA2011101801049Skin · looseRT OTD FLAP LOWER SKIN HAS LOOSE FASTENERS AT INBD END NEAR THE T/E. INSTALLED BLIND FASTENERS IAW RD 8/4-57-1659. APPLIED TOP COAT TO RIVETS.SDR GLBA20111012FStructure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND THE RT OTBD FLAP CRACKED AT LWR INBD EDGE OF THE ACCESS PANEL AREA, 6.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-120-57-002. MATERIALS UTILISDR IPXA11M70178Vane · delaminatedINSPECTION TYPE:4C RT INBD FLAP VANE LOWER SURFACE IS DELAMINATED AT XIFH 252.5. ACCOMPLISHED EA 01011-5750-01-A3515 I/R, AND EO MD11-5750-44768-A.SDR USAA2011101400026Flap · delaminatedC3 CHECK - DELAMINATION ON RIGHT WING OUTBOARD TRAILING EDGE FLAP APPROX 51 INCHES INBOARD FROM OUTBOARD END AT NR 3 FLAP TRACK. REPLACED RIGHT WING OUTBOARD TRAILING EDGE FLAP.SDR IPXA11669821Wedge · delaminatedINSPECTION TYPE: 8C, LT WING OTBD T/E FLAP, T/E WEDGE MID AREA LWR SURFACE DELAMINATION. FIBERGLASS PREPERG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR5 A (1), FIG 9, REV 50.SDR UALA2011101205545Cap · damagedAPPEARS TO BE A BIRD STUCK IN LEFT WING FLAPS OUTBOARD OF ENGINE. REMOVED AND REPLACED L/E FLAP CAP.SDR SWAA116985Skin · delaminatedDURING SCHEDULED 28Y CHECK, FOUND LT WNG I/B MID FLAP I/B UPPER SURFACE DELAMINATED. REPAIRED MID FLAP IAW SRM.SDR A6WA201141035Skin · dentedDENT WITH TWO GOUGES LT FLAP LOWER SURFACE INBD HINGE ARM. REPAIRED IAW REO 601R-52-1792.SDR LR7A2011101100238Skin · crackedDURING SCHEDULED B-3, CHECK IAW JOB CARD HB2703 FOUND LT INBD FLAP UPPER SKIN CRACKED AT CWS120 BUMPER PAD AREA. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-12.SDR FDEA201110094393Spar · crackedRT WING, INBD FLAP, MOST INBD NR 2 HINGE AREA HAS REAR SPAR CHORD CRACKED AT CUT-OUT. CUT OUT DAMAGED SECTION OF SPAR IAW SRM 51-40-4 FIG 3. FABRICATED NEW SPAR SECTION AND SPLICE IAW SRM 51-40-4 FIG 3 AND 57-50-2 FIGURE 5. TREATED, PRIMED AND INSTALLED NESDR FDEA201110094392Spar · crackedRT WING, INBD FLAP, MID FLAP, MOST INBD NR1 HINGE AREA HAS REAR SPAR CRACKED AT CUT-OUT. REPAIRED SPAR.SDR FDEA201110094389Skin · puncturedLT WING INBD FLAP LWR SKIN JUST AFT OF THE CARRIAGE FOUND PUNCTURED. CUT OUT THE DAMAGED LOWER SKIN PER SRM 57-52-12/201 FIG205.SDR SWAA116966Flap · delaminatedRIGHT WING I/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED T/E FLAP IAW MM.SDR CA111012011Spindle · sheared(CAN) ACFT WAS ON FINAL APPROACH, WHEN THE FLIGHT CREW SELECTED INCREASING FLAP ANGLES, THEY NOTICED THE ACFT TENDED TO ROLL TO THE LT AND RUDDER TRIM WAS REQUIRED TO STABILIZE THE ROLL. WITH FLAPS SELECTED TO 40, 3 UNITS OF RUDDER TRIM WERE REQUIRED TO COMPESDR A6WA201141090Roller · chafedRT WING FLAP ROLLER FITTING IS CHAFED. BLENDED CHAFED AREA AT RT WING FLAP ROLLER FITTING IAW REO 601R-57-51-143. ROTO PEENED AREA IAW REO 601R-57-51-143.SDR A6WA201141087Fairing · crackedLT OTBD CENTER HINGE ARM FLAP FAIRING GUIDE CRACKED, R & R.SDR USAA2011102700011Skin · debondedC1 CHECK - AREA OF DISBOND ON RIGHT INBOARD AFT FLAP UPPER SKIN BETWEEN IFS118.25 IFS129. REPAIRED RIGHT INBOARD AFT FLAP UPPER SKIN BETWEEN IFS118.25 IFS129 IAW B767 SRM 51-70-10-2R REPAIR 4.SDR A6WA201141091Vane · chafedRT INBD FLAP VANE CHAFED ON L/E. BLENDED AREAS ON RT INBD FLAP VANE IAW REO 601-57-52-004 AND SRM 51-12-00. TREATED AREA IAW SRM 51-21-16 AND SRM 51-25-26.SDR USAA2011102700009Skin · delaminatedC1 CHECK - DELAMINATION ON RIGHT WING OUTBOARD FLAP BOTTOM SKIN AT WS 815.5. REPAIRED RIGHT WING OUTBOARD FLAP BOTTOM SKIN AT WS 815.5 IAW B767 SRM 51-70-17-0G FIGURE 10.SDR FDEA201110074370Skin · damagedRT WING INBD UPPER FLAP SKIN MISREPAIRED IAW SRM 57-50-00, FIG 205 REPAIRED IAW SRM 57-50-00, FIG 205, PG 219.SDR FDEA201110074381Skin · chafedRT WING INBD FLAP, MOST INBD T/E UPPER SURFACE HAS A 2.5 " X .1 " X .002" CHAFE MARK. SMOOTHED & BLENDED CHAFE MARK IAW SRM 51-73-10 ORIGINAL THICKNESS OF .012 AFTER .008 FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00, FIG 101. R & R SKIN ASSY AT RT INBD FLAP T/SDR A6WA201140948Guide · out of positionLEFT OTBD FLAP CENTER HINGE ARM OTBD FAIRING GUIDE IS CHAFING THE BUTTE DOOR ACTUATOR. R & R FAIRING GUIDE BRACKET LT OTBD FLAP CENTER HINGE OTBD SIDE WITH SERVICEABLE PART IAW SRM 51-42-06, 51-40-06 AND 51-24-21.SDR A6WA201140950Vane · chafedRIGHT INBD FLAP VANE CHAFED 3 PLACES BLENDED AND SMOOTHED CHAFING WO IAW REO601R-57-52-004.SDR A6WA201140949Vane · chafedLEFT INBD FLAP VANE CHAFED 3 PLACES BLENDED AND SMOOTHED CHAFING IAW REO 601R-57-52-004.SDR DALA1157740187Skin · dentedRT WING I/B AFT FLAP AT I/B LWR SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED AS PER B767-300 SRM 57-53-01 REPAIR I FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.SDR FDEA201110064346Skin · crackedCRACK RT CENTER FLAP UPPER SKIN BETWEEN RIBS 11 AND 12 REPAIRED IAW SRM 57-50-00 FIG 205, EA 6-5750-153027.SDR CA111005008Spring · broken(CAN) A SPRING THAT KEEPS THE FLAP IN THE UP AND LOCKED POSITION WAS FOUND BROKEN DURING REGULAR MX. THE FAILURE OF THIS SPRING HAS THE POTENTIAL TO CAUSE THE ACFT TO LOSE CONTROL DURING FLIGHT, PARTICULARLY WHILE INVERTED.SDR IPXA11169725Bullnose · chafedINSPECTION TYPE:1C, RT WING INBD FLAP INBD BULLNOSE CHAFED. REPAIRED RT WING INBD FLAP INBD BULLNOSE BETWEEN RIBS 1 AND 2 REF STA, SA, EA 300-5750-01-A3511 AND EO A300-5750-44656-A.SDR FDEA201110054314Skin · gougedLT WING INBD FLAP UPPER SURFACE GOUGED. LOCATED 24.5 IN. FROME OTBD END AND 22 IN AFT OF LEADING EDGE. GOUGE MEASURES 1.6IN. X .3IN. X .007IN. BLENDED GOUGED SKIN AND REPAIRED IAW EA 6-5750-156025.SDR FDEA201110054300Access Panel · gougedGOUGE - LT INBD FORE FLAP L/E ACCESS PANEL, UPPER SURFACE, APPROX FLAP CENTER LINE. REMOVED & REPLACED LT INBD FOREFLAP ASSY IAW MM 27-51-001-4. OPS CHECKED NORMAL IAW MM 27-51-000-5.SDR FDEA201110054317Bracket · brokenRT WING CENTER FLAP OTBD CLOSING RIB 16 HAS A BROKEN ANGLE BRACKET. R & R 1 EA ANGLE BRACKET ON RT WING CENTER FLAP OTBD CLOSING RIB 16 IAW SRM 51-40-21 PG 7 A (1).SDR EE4Y20111005010Fitting · corrodedRT WING REAR SPAR AT RSS 436 AND RSS 260 AND LT WING AT RSS 260 FLAP TRACK FITTING OTBD HOLES CORRODED. THE PARTS DAMAGED WERE REPLACEMENT, WO Z10226, ITEM'S 6-90, 5-96, 6-89.SDR A6WA201141037Lug · chafedAFT LUGS FOR RT INBD HINGE ARM ATTACH POINTS ARE GOUGED AND CHAFED BLEND AREA IAW REO 601R-57-52-1536.SDR USAA2011100600026Skin · delaminatedC6 CHECK - DELAMINATION ON RIGHT WING INBOARD AFT FLAP 12.5 INCHES INBOARD OF OUTBOARD EDGE ON UPPER & LOWER SURFACES. REPLACED RIGHT WING INBOARD AFT FLAP IAW B737 AMM 27-51-11.SDR DALA1156690138Skin · dentedINBOARD AFT FLAP LWR SURFACE DENTED. METAL HOT BOND REPAIR C/W PER B767-300 SRM 57-53-01, REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.SDR CA120215003Control Rod · used(CAN) LT AND RT OUTBOARD FLAP CONNECTING RODS FOUND RUBBING ON TRAILING EDGE WING RIBS AT WS 140 .SDR A6WA201141036Vane · chafedLT INBD FLAP VANE CHAFED WHERE IT CONTACTS STOP, BLEND CHAFED AREA WITHIN ALLOWABLE LIMITS.SDR A6WA201141038Vane · chafedRIGHT INBD FLAP VANE CHAFED WHERE IT CONTACTS STOP. BLEND CHAFED AREA WITHIN ALLOWABLE LIMITS.SDR SWAA116896Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REMOVED AND REPLACED AFT FLAP PER MM.SDR CA111004009Attach Bracket · cracked(CAN) DURING PRE-FLIGHT WALK AROUND THE PILOT FOUND THE RT FLAP, INBD FLAP ATTACH ARMS SEVERELY BUCKLED. DURING THE PREVIOUS FLIGHT THE PILOT REPORTED THAT HE WAS PERFORMING A NR OF SLIPPING DESCENTS ACCOMPANIED BY PRECAUTIONARY LANDINGS AFTER HE NOTICED A CLSDR UALA2011100305347Skin · puncturedRIGHT INBD MAIN FLAP UPPER SURFACE HAS SMALL PUNCTURE. LOCATED 32 INCHES FROM INBD END & 3.5 INCHES FWD OF T/E. REPAIRED PER SRM. RESTORED FINISH.SDR HALA2011100100421Skin · damagedACFT EXPERIENCE A LIGHTING STRIKE AFTER TAKEOFF. FOUND LIGHTING STRIKE DAMAGE ON TOP SURFACE OF RT OTBD FLAP ABOVE OTBD FAIRING, AND LIGHTING STRIKE EXIT DAMAGE ON LT WINGLET T/E TOP. PERFORMED HAL-M251-767 INSP OF ACFT & OPS CK OF RADIO & NAVIGATION SYS. RSDR CA111003003Flap Track · sheared(CAN) THE FWD LOWEST HORIZONTAL RIVET ATTACHING THE RT WING INBD FLAP RAIL (PN 0523231-13) WAS FOUND TO BE SHEARED DURING INSPECTION. WITH SLIGHT UPWARDS PRESSURE ON THE FLAP, WITNESSED THE RIVET HEAD FLEX IN AN ABNORMAL WAY WITH SLIGHT MOVEMENT AND SHOWINGSDR USAA2011111000012Link · crackedS2 CHECK - CRACK IN LEFT WING NR 3 FLAP TRACK REAR LINK ASSEMBLY AT WS 9184 BETWEEN RIB 13 & RIB 14. REPLACED LEFT WING NR 3 FLAP TRACK REAR LINK ASSEMBLY IAW A330 AMM 27-54-75.SDR UALA2011100305316Skin · wornLEFT INBOARD TRAILING EDGE MAIN FLAP HAS A DEEP WEAR MARK IN THE UPPER SURFACE AT APPROX MFSTA 298. INSTALLED DOUBLER REPAIR PER ECRA5721-01318 AND EVA 81348. MAJOR REPAIRSDR UALA2011092905281Panel · crackedRIGHT WING INBOARD MID FLAP, LEADING INBOARD EDGE ADJACENT TO ACCORDIAN SEAL FLAP HAS APPROX 2 INCH X 2 INCH. PUNCTURE OR EROSION DAMAGE. STARTED PERMANENT REPAIR REF SERVICE TIP MM. NEED TO COMPLETE REPAIR FROM STEP C8 PAR C AFTER CURE IS COMPLETE. NEED TO
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