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 A6WA201140967Vane · chafedLT INBD FLAP VANE CHAFED 3 EA PLACES. REPAIRED IAW REO 601R-57-52-004 AND SRM 57-42-13.SDR DALA1161751703Flap · dentedTWO DENTS ON THE RIGHT I/B TRAILING EDGE FLAP UNDERNEATH. DENTS MEASURE ARE 4 INCH WIDTH AND 0.05 DEEP. SECOND DENT 3 INCH WIDTH AND 0.04 DEEP. PERFORMED METAL HOT BOND REPAIR PER B767-300 SRM 51-70-10 REPAIR 4 FIG 201 AND SRM 57-53-01 REPAIR 1 FIG 201.SDR KCSA111255Spar · corrodedRIGHT I/B FLAP FWD FACE OF AFT SPAR INSIDE PANEL 678GT CORRODED 2" FROM I/B END - FOUND TO BE OUT OF LIMITS.SDR KCSA111253Flap · corrodedRIGHT I/B AFT FLAP LWR FWD EXT 135" FROM O/B END CORROSION ALONG PANEL SEAM - FOUND TO BE OUT OF LIMITS.SDR USAA2011111500007Skin · debondedC3 CHECK - DEBONDING ON RIGHT WING INBOARD MAIN FLAP UPPER SURFACE 39 INCHES OUTBOARD OF INBOARD END, 18 INCHES UP FROM AFT TRAILING EDGE. REPAIRED RIGHT WING INBOARD MAIN FLAP UPPER SURFACE IAW EA 103480.SDR FDEA201111034743Skin · dentedLT WING INBD FLAP INBD L/E RIB HAS A 1" X 1" X .102" DENT REPAIRED LT WING INBD FLAP INBD L/E DENT IAW WITH SRM 57-50 00, PG 231-234, FIG 208.SDR QXEA2011111001207Skin · chafedRT OTBB FLAP CHAFED ON UPPER SKIN. BLENDED CHAFED AREA YW 194.5 TO 210, 15 INCHES FWD OF T/E OF RT INBD FLAP, WIDTH OF BLEND WAS .375/.002 MATERIAL REMOVED. BLENDED CHAFED AREA YW 227 TO 244 APPROX 13.5 INCHES FWD OF T/E OF FLAP, DEPTH OF BLEND WAS .004. BOSDR SWIA201128571Vane · chafedLEFT INBOARD FLAP CENTER VANE LEADING EDGE CHAFED. (C-CHECK) REPLACED LEFT INBOARD FLAP CENTER VANE LEADING EDGE.SDR FDEA201111024720Vane · delaminatedLT WING OTBD FLAP VANE TOP SURFACE FOUND DELAMINATED. VANE R & R IAW AMM 27-50-32-4, REVISION 70.1. FLAP VANE ADJUSTED AND TEST CARRIED OUT IAW AMM 27-50-32-5, REVISION 70.1. FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.SDR A6WA201141065Vane · chafedRT INBD FLAP VANE CHAFED 2 EA PLACES. BLENDED OTBD CHAFED AREA, ALODINED, PRIMED AND TOP COATED AND APPLIED TEFLON COATING IAW REO 601R-57-52-004. REMOVED INBD L/E SKIN, INSTALLED NEW SKIN PN 601R14303-54 AND TOP COATED IAW SRM 51-42-13, 51-23-00, 51-25-16.SDR IPXA11170366Skin · gougedINSPECTION TYPE:4C, LT INBD FLAP NOSE AND UPPER SKIN FWD OF STGR 2.2 AND BETWEEN RIBS 3 AND 4 HAS 10 EA GOUGES. REPAIRED LT INBD FLAP NOSE AND UPPER SKIN FWD OF STR 2.2 AND BETWEEN RIBS 3 AND 4 HAS 10 EA GOUGES IAW EO A300-5750- 45129-A AND STA-SA EA 300-5750SDR IPXA11170358Skin · gougedINSPECTION TYPE:4C, LT WING CENTER FLAP UPPER SKIN BETWEEN RIBS 21 AND 23, STRINGERS 2.6 AND 2.7, EXISTING REPAIR DOUBLER IS GOUGED. REPAIRED LT WING CTR FLAP UPPER SKIN BETWEEN RIBS 21 AND 23, STRINGERS 2.6 AND 2.7 IAW STA-SA EA 300-5750-01-A3596-I/R AND EO SDR IPXA11170354Skin · gougedINSPECTION TYPE:4C, LT WING CTR FLAP REPAIR DOUBLER IS GOUGED BETWEEN RIB 13 AND RIB 15 STR 2.6 AND STGR 2.8. ACCOMPLISHED REPAIR ON LT WING CTR FLAP BETWEEN RIB 13 AND RIB 15, STGR 2.6 AND STR 2.8 IAW EO A300-5750-45089-A, PARA 6A.SDR IPXA1B70218Skin · delaminatedINSPECTION TYPE:3C, LT WING OTBD FORE FLAP L/E DELAMINATED. REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1), FIG 5, REV 60.SDR UALA2011110205934Structure · missingBOTH INBD FLAPS ELEPHANT EARS MISSING. PARTS NOT AVAILABLE MCO. -INF- :PARTS ORDERED AT MCO. 28 EA BACB30NN3K14, 2 EA 113N2038-7, 2 EA 113N2038-8, 1 EA 113N2037- 9SP, 1 EA 113N2037-10SP, AND 2 EA 113N2039-1. RPL- :INSTALLED, ADJUSTED AND OPS CHECKED PER BOEISDR IPXA11170327Skin · chafedINSPECTION TYPE:4C, RT WING OTBD FLAP BULLNOSE SKIN IS CHAFED BETWEEN RIB 1 AND RIB 2. ACCOMPLISHED REPAIR IAW EO A300-5750-45028-A PARA 6A.SDR IPXA11670303Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1), FIG 5, REV 5.1.SDR VNAA2011103000036Skin · dentedDURING SCHEDULED MAINTENANCE A SMALL DENT ON THE RT INBOARD LOWER FLAP SKIN WAS FOUND DENTED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR UALA2011103105898Fairing · damagedINBOARD FLAP FAIRING ON LEFT WING NOT LINING UP. REMOVED AND REPLACED FAIRING, INSTALLED FAIRING PER MM.SDR NSVA2011282Skin · corrodedPREVIOUSLY INSTALLED DOUBLER REPAIR TO LT FUSELAGE NOT IN THE DAMAGE LOG. THE DOUBLER WAS FIRST INSTALLED IN OCTOBER 1997 (REF SAAB STATEMENT 72SD0721 DATED 10/27/1997) AND AGAIN 4/8/2000. REF SAAB DOC#72LKS3079 & THE PRINCIPLES OF THE SRM 53-70-10 PG 215. FSDR JR2R2011103000535Skin · chafedRT INBD FLAP LWR SURFACE CHAFED FROM PANELS 683BB & 686BB. REPAIRED IAW RO CRJ7-57-0231 & CRJ7-57-232.SDR USAA2011111100012Flap · debondedC1 CHECK - DEBONDED ON RIGHT AFT OUTBOARD FLAP 3.7 INCHES FORWARD OF TRAILING EDGE, 70.5 INCHES INBOARD OF OUTBOARD EDGE. REPAIRED RIGHT AFT OUTBOARD FLAP IAW B757 SRM 51-70-04, 57-53-01.SDR DALA1162121703Fairing · delaminatedRIGHT WING I/B MAIN FLAP O/B LEADING EDGE MAIN FLAP O/B LEADING EDGE FAIRING DELAM. COMPOSITE REPAIR CARRIED OUT AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.SDR DALA1162111703Fairing · delaminatedLEFT WING O/B FLAP LEADING EDGE FAIRING FOUND DELAMINATED AT I/B OF NR 1 FLAP TRACK AREA. COMPOSITE HOT BOND REPAIR CARRIED OUT AT DELAM AREA AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.SDR DALA1162101703Fairing · delaminatedLEFT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.SDR DALA1162091703Fairing · delaminatedLEFT WING O/B FLAP LEADING EDGE FAIRING FOUND DELAMINATED AREA AT O/B OF NR 2 FLAP TRACK AREA. COMPOSITE HOT BOND REPAIR CARRIED OUT AT DELAM AREA AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.SDR A6WA201141062Vane · chafedLT INBD FLAP VANE L/E CAPS CHAFED INBD 601R14303-53 CENTER 601R14303-39, OTBD 601R14303-43. REPLACED INBD IAW SRM 51-42-13. REPAIR OTBD AND CENTER IAW REO 601R-57-52-004.SDR UALA2011102705811Attach Fitting · defectiveLEFT WING OUTBOARD FLAP OUTBOARD FLAP TRACK, UPPER ATTACH FITTING TO FLAP MISSING 2 EACH MOUNT BOLTS. REF BOEING CMM 57-53-76, IPL FIGURE 1, SHEET 11 OF 18, ITEM'S 470 AND 473, 2 LOWER HI-LOKS. REMOVED FLAP AND INSTALLED MISSING FASTENERS, REFERENCE NON ROUTSDR SWAA117422Flap · delaminatedDURING SCHEDULED OTS CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR SWAA117391Wedge · puncturedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B AFT FLAP WEDGE PUNCTURED. REMOVED AND REPLACED WEDGE IAW MM.SDR UALA2011102405765Structure · damagedRIGHT INBD TRAILING EDGE FLAP DAMAGED. RT IB AFT FLAP WAS REPAIRED. REINSTALLED FLAP.SDR SWAA117273Skin · puncturedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN PUNCTURED AT I/B END. REPAIRED SKIN IAW SRM.SDR IPXA1569931Wedge · delaminatedLT WING INBD MAIN FLAP T/E WEDGE INTERIM REPAIR STA 300.38 REQUIRES IAW REPAIR. REPAIRED IAW EO B757-5750-36938-E AND SRM 57-53-01-2R, REPAIR 1.SDR AALA20111021TUL19Skin · delaminatedOUTBOARD AFT LEFT FLAP HAS DELAMINATION ON BOTTOM SIDE APPROXIMATELY 12 INCHES FROM OUTBOARD END. BONDED AND SANDED ALL CORES AND SKINS. COMPLETED HOT BOND REPAIR PILES PER SRM 51-70-04-0G.SDR FDEA201110214614Skin · crackedRT WING OTBD FLAP UPPER SURFACE 21" FROM THE OTBD EDGE HAS 3EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE CRACKS AT 21" FROM OTBD EDGE IAW SRM 57-10-00, FIG 6 , SH 1-3. MAJOR REPAIR.SDR FDEA201110214613Skin · crackedRT WING OTBD FLAP UPPER SURFACE STA XORS 587 HAS 2 EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE AT STA XORS 587 IAW SRM 57-10-00 VOL 1,FIG 85 SHEET 3. MAJOR REPAIR.SDR DALA1159346313Flap · damagedLT WING I/B FLAP CORNER COMPOSITE DAMAGE. REMOVED AND REPAIRED FLAP DAMAGE, HOT BONDED AND VACUUM BAGGED REPAIR, SANDED AND PAINTED REPAIR REF SRM 51-70-07. OK FOR SERVICE.SDR USAA2011102400010Flap · debondedC4 CHECK - AREA OF DISBONDING ON RIGHT INBOARD AFT FLAP APPROX 12 INCHES FROM INBOARD END ON LOWER SURFACE. REPLACED RIGHT INBOARD AFT FLAP ASSEMBLY IAW B737 AMM 27-51-11.SDR IPXA11170120Structure · chafedINSPECTION TYPE:3C, LT WING OTBD FLAP INBD BULLNOSE CHAFED. REPAIRED LT WING OTBD FLAP INBD BULLNOSE BETWEEN RIB 1 AND 2 REF EA 300-5750-01-A3574 AND EO A300-5750-44874-A.SDR USAA2011102400009Exhaust Gate · delaminatedC4 CHECK - 1 INCH AREA OF DELAMINATION ON LEFT WING OUTBOARD EXHAUST GATE. REPLACED LEFT WING OUTBOARD EXHAUST GATE IAW B737 AMM 27-51-35.SDR SWAA117226Flap · puncturedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B MAIN FLAP L/E PUNCTURED. REMOVED AND REPLACED MID FLAP PER MM.SDR FDEA201110194586Flap Track · gougedRT WING NR3 FLAP TRACK OTBD FACE HAS INDENTATIONS AT FWD AND AFT SECTION. SECTION (EA MEASURING L=1" X W=0.25" X D=0.05") R & R RT NR3 FLAP TRACK BEAM IAW AMM 57-20-24-4. REMOVED ANR RE-INSTALLED NR3 FLAP TRACK CARRIAGES IAW AMM 27-54-27-4 TO FOM. REMOVED ANSDR IPXA11569794Skin · dentedINSPECTION TYPE:C3, LT INBD MAIN FLAP UPPER SURFACE SKIN PANEL IS DENTED AT 103" OTBD OF THE INBD END WITH DELAMINATION NOTED. R & R DELAMINATED SKIN AND CORE IAW 757-200PF SRM 51-70-10-2R.SDR FDEA201110184575Carriage · damagedRT WING NR 2 FLAP TRACK CARRIAGE AFT OTBD YOKE ROLLER DAMAGED. R & R NR 2 FLAP TRACK CARRIAGE AFT OTBD YOKE ROLLER IAW AMM 20-21-12.SDR SWIA201130834Vane Cap · chafedLEFT INBOARD FLAP INBOARD VANE CAP CHAFED. (C-CHECK) REPAIRED PER REO.SDR FDEA201110170302Skin · dentedLEFT INBD FLAP LOWER SURFACE HAS DENTS JUST INBD OF THE OTBD HINGE. FOUND DENT OUT OF LIMITS AND REPAIRED LT INBD FLAP LOWER SURFACE SKIN IAW SRM 57-10-00, FIG 85, CLASSIFIED AS MAJOR REPAIR.SDR FDEA201110174550Skin · gougedLEFT WING CENTER FLAP UPPER SURFACE CHAFED & GOUGED. GOUGES APROXIMATELY .2500" DIA X .040" DEEP. REPAIRED IAW SRM 57-50-00 PB 201 PARA 4F.SDR QXEA2011101901079Flap Track · corrodedRT WING NR 4 FLAP TRACK IS CHAFED IN 2 PLACES ON INBD VERTICLE FACE. BLENDED DAMAGE IAW RD 8/4-57-1238. MINIMUM REMAINING THICKNESS .145, CONFIRMED AREA TO BE CRACK FREE. COMPLETED REPAIR IAW RD 8/4-57-1238.SDR SWAA117142Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR UALA2011101405581Seal · looseRT WING FLAPPER SEAL LOOSE AND HANGING DOWN. MISSING 3FT OF SEAL ON INBD FLAPERON. FOUND ELEPHANT EAR SEAL WORN OUT. REPLACED SEAL.
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