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 ASAA0843442Skin · dentedRIGHT I/B MID FLAP LOWER SURFACE T/E WEDGE HAS MULTIPLE SMALL DENTS BETWEEN MIDDLE TRACKS. REPAIRED RIGHT I/B MID FLAP WEDGE LOWER SURFACE DENTS IAW B737 400 SRM 51-30-01 PG 13.SDR ASAA0843441Skin · dentedLT WING I/B MID FLAP TRAILING EDGE WEDGE HAS 3 EA SHARP DENTS ON LOWER SURFACE 46 INCHES FROM I/B END. REPAIRED LT WING TRAILING EDGE WEDGE MID FLAP IAW B737 400 SPM 51-70-10 REPAIR 4.SDR ASAA0843440Skin · dentedRIGHT I/B FORE FLAP LOWER SURFACE ABOVE NR 4 TIRE IS PUNCTURED AT ONE DENT IN THE MIDDLE OF A GROUP OF DENTS. REPAIR RIGHT I/B FORE FLAP LOWER SURFACE IAW B737 400 SRM 51-70-10.SDR ASAA0843439Skin · dentedLT WING I/B FORE FLAP UPPER SURFACE HAS A SMALL DENT 53 INCHES O/B FROM I/B END AND .75 INCHES UP FROM TRAILING EDGE. REPAIRED LT WING I/B FORE FLAP UPPER SUFRACE IAW B737 400 SRM 51-70-10 REP 2 PG 201.SDR ASAA0843438Skin · delaminatedLT WING I/B FOR FLAP REPAIR ON UPPER SURFACE 34 INCHES FROM O/B AND CHAFED AND DELAMINATED. REPAIRED DAMAGE TO LT WING I/B FORE FLAP UPPER SURFACE IAW B737 400 SRM 51-70-10 PARA 96 PG 217 REPAIR 4.SDR 08FDEA03707Skin · dentedFOUND SEVERAL DENTS AND IMPACTS ON RT INBOARD FLAP, LOWER SURFACE THREE DOUBLER REPAIRS (RIB 9-11, 12-16, 12-15) WERE PERFORMED IAW RAS/FOK/233/2008 ISS.C, APPROVED BY EA 6-5752-123073.SDR 08FDEA03705Skin · damagedFOUND OLD DOUBLER REPAIR NOT PERFORMED IAW RAS/FOK/138/98 (TOP AND LOWER DOUBLER), LOWER DOUBLER MISSING, RIB 17A-18 TRAILING EDGE. DOUBLER REPAIR RENEWED IAW RAS/224/2008 ISS.A, APPROVED BY EA 6-5752-123082.SDR 08FDEA03684Fitting · crackedRIGHT WING INBOARD FLAP; OUTBOARD END; FOLLOW UP GUIDE FITTING IS CRACKED. REMOVED GUIDE FITTING IAW SRM 51-40-02; PG 1 & DRILLED NEW FITTING 1AW SRM 51-40-40 PG 2. INSTALLED NEW FITTING IAW SRM 51-40-02; PG 1.SDR 08FDEA03683Fitting · crackedLEFT WING INBOARD FLAP OUTBOARD END; FOLLOW UP GUIDE FITTING IS CRACKED. REMOVED & INSTALLED FITTING IAW SRM 51-40-30. LOCATED & DRILLED IAW SRM 51-40-40. PAINTED IAW SRM 51-23-10.SDR 08FDEA03654Vane · delaminatedRT WING INBOARD FLAP VANE LOWER SURFACE INBOARD OF MID WAY TO LEADING EDGE AREA FOUND DELAMINATED. REPAIRED IAW EA 1-5750-124362, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA03653Vane · delaminatedLT WING INBOARD FLAP VANE INBOARD OF MID WAY TO TRAILING EDGE AREA FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 08FDEA03647Skin · crackedCRACK ON DOUBLER AT RIGHT O/B FORE FLAP BY O/B TRUCK ATTACH FITTING AT WS 629. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PARTS, IAW SRM 57-50-4 FIG 7 AND 457-50-2 FIG 4. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-3SDR USAA920081601Flap · delaminatedCLT C5 MAJOR REPAIR NR 03C10025001/002 LT HAND OUTBOARD FORE FLAP DELAMINATED. REPLACED LT HAND OUTBOARD FORE FLAP IAW B737 SRM 57-53-01 & B737 AMM 27-51-37.SDR 08FDEA03639Panel · chafedLEFT WING OUTBOARD FLAP; INBOARD FAIRING; OUTBOARD SIDE PANEL 535 DL IS CHAFED ON THE INNER SKIN. BLENDED GOUGE; FOUND TO BE OUT OF LIMITS; PREPPED AREA FOR REPAIR; TREATED 7 PRIMED; FABRICATED DOUBLER; LATED UP HOT BOND REPAIR & CURED; SEALED EDGES & PRIMEDSDR 08FDEA03638Panel · gougedRIGHT WING OUTBOARD FLAP FAIRING INBOARD SIDE PANEL 635 GL HAS A GOUGE. BLENDED GOUGE; FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-52-01; VOL III & SRM 57-00-01; VOL I. PREPPED SURFACE; TREATED & PRIMED; FABRICATED DOUBLER; LAYED UP HOT BOND REPAIR & CURESDR 08FDEA03642Vane · delaminatedLEFT OUTBOARD FLAP VANE; INBOARD LOWER SKIN IS DELAMINATED. REMOVED DELAMINATED INBOARD LOWER SKIN ON LEFT OUTBOARD FLAP VANE INBOARD END. FABRICATED SKIN PLUG & REPAIR DOUBLER. PREPPED FOR BONDING; HOT BONDED REPAIR. ALODINED AREA & EDGE SEALED DOUBLER;SDR 08FDEA03616Spar · crackedRT WING O/B MID FLAP AFT SPAR, UPPER CHORD IS CRACKED AT WBL 332 REMOVED AND REPLACED RT O/B MIDFLAP ASSY IAW FX B727-200 MM 27-51-011-4. OPS CHECK GOOD IAW FX B727-200 MM 27-51-011-4 AND 27-51-000-5.SDR 08FDEA03617Skin · chafedLT WING O/B FORE FLAP L/E REPAIR DOUBLER IS CHAFED (DAMAGED) AT WS 440 REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 57-50-2 FIG 4 AND SRM 57-50-4 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM SDR 08FDEA03618Flap Track · wornRIGHT WING FLAP FAIL SAFE BOLT PIN PLATING IS WORN, (FWD BOLT). REMOVED AND REPLACED THE RIGHT WING INBD FLAP FAIL SAFE BOLT REF AMM 57-20-24-4.SDR SWAA084775Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP PER MM.SDR SWAA084773Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR SWAA084750Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR SWAA084747Skin · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING OUTBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR SWAA084746Skin · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.SDR C8GA20080052Skin · gougedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT IB FOREFLAP AT THE UPPER SURFACE HAS A 10" GOUGE. REMOVED DAMAGED SKIN, FABRICATED CORE. FABRICATED DOUBLER. HOT BONDED CORE AND DOUBLER SEALED EDGES IAW SRM 51-40-20. NO OTHER DEFECTS NSDR UALA2008111305461Flap · puncturedLEFT INBOARD FORE FLAP LEADING EDGE HAS A LARGE PUNCTURE. FOUND PUNCTURED FORE FLAP DAMAGED FROM TIRE TREAD. REPAIRED DAMAGED SPAR PER SRM 51-70-12, REPAIR 1. REPAIRED LOWER PANEL ON R61502 PER SM-80-57-53-17-JD. REPAIRED L/E BULLNOSE ON R61505 PER SRM 57-SDR USAA920081754Skin · delaminatedSAL - MAJOR REPAIR - C17 CHECK, DELAMINATING ON RT WING INBOARD FOREFLAP UPPER SURFACE, WBL 73- WBL 184.275. REPAIRED RT WING INBOARD FOREFLAP UPPER SURFACE, WBL 73- WBL 184.275 IAW B737-300 SRM 51-10-2RSDR 2008UALA05461Skin · puncturedLEFT INBOARD FORE FLAP LEADING EDGE HAS A LARGE PUNCTURE. REMOVED LEFT INBOARD FORE FLAP. COMPLETE FORE FLAP INSTALLATION FROM ITEM 3 PAGE 407 TO COMPLETION.SDR SWAA084711Skin · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING OUTBOARD T/E FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR ASAA0843420Skin · dentedDENT 1 AND 2 (WBL 87.5 AND WBL 87.8) FOUND BEYOND ALLOWABLE LIMITS IAW B737 400 SRM 57 53 02. TRANSFERRED FROM MIG5 NR 5106400 LT INBOARD MID FLAP T/E WEDGE. LT INBOARD MID FLAP T/E WEDGE REPAIRED IAW B737 400 SRM CH 51 70 10.SDR ASAA0843456Skin · dentedLEFT INBOARD MIDFLAP T/E WEDGE HAS DENTS NEXT TO A PREVIOUS REPAIR. REMOVED DAMAGE, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2.SDR ASAA0843458Skin · dentedLEFT INBOARD FOREFLAP LOWER SURFACE HAS MULTIPLE SHARP DENTS. PREPPED DAMAGED AREA, FABBED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2.SDR ASAA0843455Skin · delaminatedNR 1 SLAT LOWER T/E SURFACE IS DELAMINATED AT THE OUTBOARD CORNER. REMOVED DELAM SKIN AND CORE FABBED REPLACEMENT CORE, SKIN AND DOUBLER. BONDED REPAIR IAW B737 400 SRM 51 70 10 8.SDR ASAA0843453Skin · dentedNR 4 SPOILER LOWER SURFACE HAS MULTIPLE DENTS IN 6 LOCATIONS. PREPPED 6 AREAS FOR REPAIRS FABBED 6 DOUBLERS AND BONDED REPAIRS IAW B737 400 SRM 51-70-10 REPAIR 2. NOTE THE 2 REPAIRS ON THE INBOAR END HAVE THE SAME DIMENSIONS WBL 87.75 92.25 ABOVE AND BELOW TSDR ASAA0843450Skin · dentedRIGHT INBOARD FOREFLAP LOWER SURFACE HAS SEVERAL DENTS OUTBOARD OF INBOARD TRACK. REMOVED DAMAGED AREA, FABBED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2.SDR USAA920081756Skin · delaminatedSAL - MAJOR REPAIR - C19 CHECK, RT WING OUTBOARD FOREFLAP UPPER SURFACE DELAMINATED, WBL 202.6 -WBL 414.4. REPAIRED RT WING OUTBOARD FOREFLAP UPPER SURFACE, WBL 202.6 - WBL 414.4 IAW B737-300 SRM 57-70-2R.SDR 08FDEA03539Skin · dentedRIGHT WING - INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 255. RIGHT WING - INBOARD FLAP LOWER SURFACE DENT AT XIFH 255 DAMAGED CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 2 VOLUME I. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR C8GA20080056Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AFT FLAP HAS 1 LARGE DENT NEAR CENTER ON BOTTOM SIDE. REMOVED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IAW SRMSDR C8GA20080055Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AFT FLAP BOTTOM SIDE UNDERNEATH TEARDROP AREA DELAMINATED. REMOVED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IASDR UALA2008111304371Skin · wornLT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN. ACP REPAIR PER 777EN57-004 7-01. THE REPAIR IS APPROVED BY BAC FORM 8100-9. THE REPAIR IS PERMANENT REPAIR. NO RE-INSPECTION IS REQUIRED.SDR UALA2008111304370Skin · wornRT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN. ACP REPAIR PER 777 EN-57-00 46-01, THE REPAIR IS APPROVED BY BAC, FORM 8100-9. THE REPAIR IS PERMANENT REPAIR.SDR 08FDEA03516Skin · dentedLEFT WING - INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 249. LEFT WING INBAORD FLAP LOWER SURFACE DENT AREAS TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA03514Skin · dentedLEFT WING - INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 130. LEFT WING INBOARD FLAP LOWER SURFACE DENT AREA TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 2008UALA04371Skin · wornLT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN.SDR 2008UALA04370Skin · wornRIGHT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN.SDR ASAA0843429Skin · dentedRIGHT WING O/B FOREFLAP DENTED 24 INCHES FROM I/B END 4 INCHES FROM T/E. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2.SDR ASAA0843427Skin · dentedLEFT WING I/B FORE FLAP UPPER SURFACE DENTED AND CHAFED 47 INCHES FROM I/B END AND 9 INCHES FROM T/E. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2.SDR ASAA0843405Skin · dentedLT WING I/B AFT FLAP DENTED ON LOWER LEADING EDGE SURFACE 46 INCHES FROM I/B END. REMOVED DAMAGED SECTION OF FLAP LEADING EDGE FABRICATED, LOCATED, DRILLED AND INSTALLED NEW LEADING EDGE SECTION IAW B737 400 SRM 57 53 01 DETAIL IV PG 4 AND B DWG 65 4634.SDR SWIA200819966Structure · crackedCRACK IN LEFT NACELLE FLAP. REPLACED LEFT NACELLE FLAP IAW EMB 120 MM 27-50-03.
SDR 08FDEA03506Skin · crackedLEFT WING INBD FLAP L/E HAS A DENT APPROXIMATELY 6' FROM THE INBD EDGE OF THE FLAP. REPAIRED THE LEFT WING INBD FLAP L/E SECTION IAW SRM 57-50-00, FIG 208.
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