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 SWAA112237Flap · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA112161Flap · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.SDR IXXA11SMN0056SSkin · dentedDURING REOUTINE C-CHECK INSP FOUND LT INBD FLAP UPPER SKIN DENTED AT STA XW 104.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPARED PARTS. INSTALLED REPAR PARTS IAW SRM CHAPTER 57-7-1, FIG 1 ITEM "D", SRM 51-1-21, SRM SDR IXXA11SMN0055SSkin · wornDURING ROUTINE C CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN WORN AT STA XF 169.000 - 213.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIRED PARTS IAW SRM CHAP 57-7-1, FIG 4 ITEM "C", DPS 4.710 SDR CALA2011032800206Flap Track · corrodedRT WING NR 7 FLAP TRACK AFT ATTACH EMITTING RUST. REPLACED FLAP TRACK REF MM 27-51-49-004-001 AND MM 27-51-49-404 -006. ROTABLE PARTS CHANGE WAS INDICATED - TT 1429471 S/N OFF 01631 TRACK, FLAP, O/B OFF 24-5753-9-9001 1631, ON 24-5753-9-9001 2569.SDR FDEA201103261183Skin · dentedRT OTBD AFT FLAP HAS 1 DENT 1.5" X 3" .093 42" FROM INBD EDGE. REMOVED DAMAGED AREA IAW SRM 57-50-4, FIG 9 AND FABRICATED REPAIR DOUBLER IAW SRM 57-50-4, FIG 9 SHEET 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.SDR UIEA2011032500174Skin · delaminatedDURING C3 CHECK OF THE DATUM ACFT, DELAMINATION DAMAGE WAS FOUND ON L/E OF THE LT OTBD MID FLAP (PN 65B01925-309C, SN 000474). DELAMINATION MEASURES 3" X 2" AND 3" X 1.5" LOCATED IN DISTANCE OF 180" AND 186" FORM INBD EDGE OF THE MID FLAP. (REPAIR WAS ACCOMPSDR UIEA2011032500164Skin · debondedDURING D2 CHECK INSP BEING PERFORMED; A DISBOND DAMAGE WAS FOUND TO THE RT WING OTBD T/E AFT FLAP UPPER PANEL INNER SKIN. DELAMINATION AREA WAS BETWEEN WING STATION, WBL 747.678 - 799.20 AND AS SHOWN IN FIGURE 2. (ALL DETAILS OF DAMAGE AND REPAIR DATA WERE RSDR IPXA11566114Flap Track · crackedINSPECTION TYPE:CK, RT MLG WHEEL WELL AFT BULKHEAD FLAP TRACK SUPPORT LINK BETWEEN FUSE LAGE AND LOWER BEAM IS CRACKED AT UPPER ATTACH BOLT AFT LUG. R & R RT FLAP INBD TRACK AFT SUPPORT VERTICAL SUPPORT LINK. NEW SUPPORT LINK WAS MFG IAW EA 110333IR. ALLSDR ASAA1149440Skin · dentedRIGHT INBOARD FORE FLAP LOWER SURFACE DENTED 42 INCHES FROM INBOARD END 5 IN FROM TRAILING EDGE. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149438Skin · dentedRIGHT INBOARD FORE FLAP LOWER SURFACE HAS SEVERAL DENTS CLUSTERED 49 INCHES FROM INBOARD END 9 INCHES FROM TRAILING EDGE. REMOVED DAMAGED AREA AND PREVIOUS REPAIR. FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149437Skin · chafedRIGHT INBOARD FORE FLAP UPPER SURFACE DOUBLER CHAFED. REMOVED DAMAGED DOUBLER FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149436Skin · gougedRIGHT INBOARD FORE FLAP UPPER SURFACE GOUGED 51 INCHES FROM INBOARD END 10 INCHES FROM LEADING EDGE. REMOVED DAMAGED SECTION FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149435Skin · chafedRIGHT INBOARD FORE FLAP OUTBOARD UPPER SURFACE CHAFED. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149431Skin · chafedLEFT INBOARD FORE FLAP UPPER SURFACE CHAFED 30 INCHES FROM OUTBOARD EDGE. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1149430Skin · chafedLEFT INBOARD FORE FLAP UPPER SURFACE CHAFED ON EXISTING REPAIR 44 INCHES FROM INBOARD END. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR UALA2011032501413Hinge Fitting · crackedLEFT WING INBOARD MAIN FLAP, TRAILING EDGE, AFT FLAP HINGE FITTING, INBOARD FLANGE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRICATED A REPAIR ANGLE AND FILLERS AND INSTALLED PER SRM.SDR SWAA112104Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP PER MM.SDR SWAA112102Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING T/E WEDGE AT I/B MID FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.SDR IPXA11M66085Skin · dentedINSPECTION TYPE:4C, RT WING INBD FLAP LOWER SKIN DENTED BETWEEN STA XIFH 133.9 & 140.6. FABRICATED & INSTALLED REPLACEMENT SKIN SECTION REF SRM 57-50-01, REPAIR 1 FIG 201.SDR FDEA201103231148Skin · dentedLT MAIN FLAP, LOWER SURFACE, DENTED. REPAIRED LT MAIN FLAP LOWER SURFACE IAW SRM 51-70-10. FINAL REPAIR DIMENSION IS APPAROX 6" IN DIAMETER. REPAIR IS LOCATED APPROX 18" OTBD OF FLAP TRACK FAIRING. MAJOR REPAIR.SDR REXA201100192Skin · dentedRIGHT INBOARD FLAP DENTED BETWEEN CANT FLAP STATION 79.062 AND CANT FLAP STATION 82.473 JUST FORWARD OF REAR SPAR ON THE UPPER SKIN. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO 601R-57-20992A AND 8110-3 DATED 3/23/11.SDR A6WA201140203Skin · chafedLT INBD FLAP VANE CHAFED ON INBD L/E. R & R PN 601R14303-535 IAW SRM 51-42-13.SDR A6WA201140206Skin · gougedRT FLAP T/E GOUGED ON LOWER SURFACE. REPAIR IAW SRM 57-52-00.SDR SWAA112059Skin · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA112004Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR CA110329010Tension Spring · broken(CAN) FLIGHT SCHOOL REPORTED ABNORMAL NOISE COMING FROM FLAPS DURING STUDENTS PRE-FLIGHT WALK AROUND INSPECTION OF CONTROL SURFACES. UPON FURTHER INSPECTION BY THE AMO, IT WAS FOUND THAT THE LOWER FLAP CABLE TENSION SPRING WAS BROKEN. SPRING WAS REPLACED AND SDR SWAA112125Flap · delaminatedDURING SCHEDULED OTS CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR FDEA201103201120Skin · crackedCRACK AT THE L/E INBD SIDE OF THE LT WING INBD FLAP FORE FLAP. REMOVED DAMAGED PANEL AT L/E LT WING FORE FLAP IAW SRM 51-30-2, FABRICATED NEW PANEL .040, 2024-O, HEAT TREATED TO T4 IAW FAS ER 2-37153-801, DRILLED TRIMMED IAW SRM 51-30-2 7 DWG 65-216-30, TREATSDR SWAA111976Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B MID FLAP I/B UPPER EDGE DELAMINATED. REMOVED AND REPLACED MID FLAP PER MM.SDR ASAA1149765Flap · delaminatedLEFT OUTBOARD FOREFLAP DAMAGED 30 IN FROM INBOARD END. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 3 AND 4.SDR A6WA201140205Skin · damagedRT OTBD FLAP, FLAP VANE L/E HAS DENT ON OTBD END. UPON EVALUATION OF RT OTBD FLAP VANE L/E ON OTBD END FOUND TO BE WITHIN LIMITS IAW REO 601R-57-53-030.SDR CALA2011032400172Skin · damagedLEFT WING NR 3 FLAP TRACK AFT FAIRING FWD I/B MOUNTING BRACKET HOLES IN FLAP ARE ELONGATED. REPAIRED MOUNTING HOLES IN FLAP AND REPLACED BRACKET PER EC/RA 5750-04368 STEPS 1 THRU 18. INITIATED DIP PER EC/RA 5750-04368 STEP 19.SDR DALA1120699870Hinge · crackedLT WING NR 3 FLAP HINGE FLAP HALF OF THE HINGE IS CRACKED. REMOVED AND REPLACED NR 3 FLAP HINGE HALF IAW CARD 5753-9893M-LT.SDR FDEA201103171058Skin · misrepairedREPAIR FOUND AT RT INBD FLAP LOWER SKIN. FOUND NOT IAW APPROVED DATA. REPAIR REMOVED AND NEW REPAIR ACCCOMPLISHED PER SRM 57-50-01 REV 46, REPAIR 1 FIG 201. COMPLIED WITH E.O. 1-5100-7-5001 A5 PART 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR IPXA1665755Fairing · 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 49.SDR DU4R2011002Skin · dentedDURING SCHEDULED INSP, FOUND RT OTBD FLAP, OTBD UPPER SKIN DENTED, CREASED DENTS.SDR DALA1119341807Support Fitting · crackedLT WING NR 3 FLAP TRACK AFT FLAP FAIRING SUPPORT FITTING CRACKED. REPAIR C/W PER ERA 490810-14AD.SDR FY4Y20110317Strap · corrodedHE CORROSION WAS FOUND AT TENSION STRAP OF LT OTBD MID FLAP AT WBL 452 DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE STRAP IS 0.225". AFTER BLEND OUT, THE DIMENSION OF THE CORROSION AREA IS 2.5" (LENGTH) X 2" (WIDTH) AND REMAINDER THICKNESS IS 0.172", IAW SDR A6WA201140230Plate · chafedRT INBD FLAP INBD HINGE LOT PLATE CHAFED. BLENDED IAW REO 601R-57-52-1536, TYPE 1 ZONE A.SDR A6WA201140193Skin · chafedRT INBD FLAP VANE L/E SKIN CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-57-52-004, REV C.SDR DALA1123101200Fairing · delaminatedRT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-03 FIG 5.SDR SWAA111857Skin · debondedDURING SCHEDULED 24Y CHECK, FOUND LEFT I/B FORE FLAP UPPER SKIN DISBONDED 46 INCHES FROM I/B END AND 8 INCHES FROM T/E. REPAIRED PER SRM.SDR FDEA201103150974Rib · crackedLT WING INBD T/E FLAP HORIZ UPPER FLANGE OF RIB 25A FOUND CRACKED RIB AT LT WING INBD T/E FLAP HORIZ UPPER FLANGE OF RIB 25A R & R IAW SRM 51-40-21, REV 74. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR CA110317002Bellcrank · cracked(CAN) DURING MX, THE PAINT, WHITE, WAS NOTICED TO BE CRACKED ON SIDE OF BELLCRANK. FURTHER INVESTIGATION REVEALED PART WAS CORRODED & CRACKED UNDERNEATH PAINT. NO IMPACT DAMAGE OBSERVED, PART REPLACED. REQUEST SENT TO HAVE PART RETURNED. FIRST OBSERVED FAISDR DALA1170460135Skin · delaminatedDELAMINATION ON UPPER SKIN. ER/A PERFORMED TO REPLACE UPPER SKIN AND CORE. ER/A 492681-14 REV A. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPSSDR USAA2011033191302Skin · debondedCLT - Q5/QX6 - DISBONDING ON LEADING EDGE OF RIGHT OUTBOARD FOREFLAP UPPER SKIN APPROX 116 INCHES INBOARD FROM THE OUTBOARD END. REPLACED RIGHT OUTBOARD FOREFLAP IAW B737 AMM 27-51-37.SDR DALA1123111200Fairing · delaminatedLT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-03 FIG 5.SDR FDEA201103140960Vane · delaminatedLEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATION. LEFT WING INBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.1. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-830-801 REVISION 69.1 SATIS.SDR AALA20110314TUL01Skin · dentedDENT IN BOTTOM OF SKIN APPROXIMATELY 6 FEET OUTBOARD OF ELEPHANT EAR FAIRING, LEFT HAND INBOARD FLAP. FABRICATED AND INSTALLED PERMANENT FLUSH REPAIR DOUBLER AND FILLER PER SRM 57-01-00, FIGURE 5 SHEET 2 AND AARD 51-60-00-05 AND SRM 51-30-02, PARAGRAPH 11.
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