JASC 5753
Service difficulty reports · 31,513
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 FDEA202202280375Skin · delaminatedFOUND RT WING OUTBOARD FLAP DELAMINATED ON TAILING EDGE 6 INCHES INBOARD OF OTBD FLAP CANOE. REMOVED DAMAGE MATERIAL CLEANED AND PREPPED AREA FOR BONDING FOR RT WING OTBD FLAP TE 6 INCHES INB OF OTBD CANOE.SDR DALA202204602377Vane · unknownPD: PUNCTURE, LOWER SKIN. INBD SLIDER MISSING. / CA: REPAIRED UNIT. THE WORK SPECIFIED IN BLOCK(S) 11/12 ACCOMPLISHED WITHREFERENCE TO OEM CMM 27-50-1, REV. 61 WITH APPLICABLE DELTA SUPPLEMENTAL INFORMATION AND CSVE, REV. 30. / ****LIMITED RELEASE: CMM 27-50-1SDR SWAA2022031078354Beam · elongatedELONGATED HOLE ON BEAM LOCATED UPPER INBOARD FIXED TRAILING EDGE RIGHT WING. 2022-55899 / [01] REPLACED BEAM LOCATED UPPER INBOARD FIXED TRAILING EDGE RIGHT WING IAW B737-700 DWG 115A2516 SHEET 5 REV- AND SRM 51-40-02;[02] REPLACED BEAM LOCATED UPPER INBOARD FSDR DALA2022051903444Vane · unknownPD: DENT ,LOWER SKIN / CA: REPAIRED PER ERA 599208-14 REV ORG.SDR SWAA2022033178414Panel · crackedLEFT WING PANEL 561BB HAS CRACKS AROUND NUMEROUS FASTENER HOLES. / [01] REPAIRED FASTENER HOLES PER SRM 51-70-04 REPAIR #9.;[02] VERIFIED REPAIR;[03] REPAIRED PER SRM 51-70-04 REPAIR #9. RESTORED FINISH PER M/M 51-21-99 AND M/M 51-21-81.;[04] INSPECTED WORK PESDR SWAA2022032878262Panel · pulledL/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES )MARKED) / VALIDATED REPAIR PER SRM 51-70-04-2R-9;[06] CURED SLURRY; SANDED SLURRY TO CONTOUR; CLEANED REPAIR AREAS; FABRICATED REPAIR PLIES FROM BMS 9-3 LOT 1475360-2; INSTALLED REPAIR PLIES WITH 9390 RESISDR SWAA2022033178156Support · crackedR/H WING LOWER T/E PANEL SUPPORT IS CRACKED AT RSS 280. (MARKED) / [01] UPDATED PARTS REQUIREMENT;[02] REMOVED AND REPLACED R/W LOWER T/E PANEL SUPPORT AT RSS 280 IAW SRM 51-40-02-0G-0;[03] VERIFIED CORRECTIVE ACTION STEP 2.SDR SWAA2022022877128Flap · delaminatedRT WING OUTBD AFT FLAP LOWER SKIN DELAMINATED AFT INBD CORNER MEASUING 7IN BY 9IN. / [01] REMOVED O/B AFT FLAP PER AMM 27-51-22.;[02] REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER AMM 27-51-22SDR IPXA2022031079938Spar · corrodedINSPECTION TYPE:C4L/H UPPER WING T/E REAR SPAR HAS CORROSION BETWEEN STA XORS=675.5 TO XORS=754.5REMOVED, REPAIRED THE CORROSION ON L/H UPPER WING T/E REAR SPAR IAW VTSAA EA 011-5710-01-A9503 REV I/R AND UPS MD11-5710-83089-A. (MINOR)SDR IPXA2022030879878Slat · damagedINSPECTION TYPE:C4L/H WING #2 SLAT T/E LWR SURFACE O/B EDGE RUBSTRIP IS DAMAGED AT STA XIS=358.005REMOVED, REPAIRED THE DAMAGED ON L/H #2 SLAT T/E RUBSTRIP IAW VTSAA EA 011-5754-01-A9499 REV I/R AND UPS EO MD11-5750-83102-A (MINOR)SDR IPXA2022030779835Skin · gougedINSPECTION TYPE:1CLT WING FIXED L/E SKIN GOUGE AT XW 290.5.REMOVED,FABRICATED AND REPLACED GOUGED SKIN IAW MD-11 SRM 51-31-01 ND DWG ARB2386-5 (MINOR).SDR AALA202204284321Flap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUT BOARD TRAILING EDGE FLAP AT RIB 11. REPLACED FLAP PER AMM 27-54-62-400-001-A,SDR SWAA2022030876509Flap · delaminatedLEFT WING OUTBOARD AFT FLAP DISBONDED ALONG I/B T/E / [01] REMOVED LEFT WING OUTBOARD AFT FLAP PER AMM 27-51-22-000-801 STEP2C(4)-2D(3)(F).;[02] INSTALLED SERVICEABLE LEFT WING OUTBOARD AFT FLAP PER AMM 27-51-22-400-801 STEP 3F(4)-(5) AND 3G(10). VERIFIED TORQSDR CALA2022022200489Seal · brokenPDA 3 LEFT WING OUTBD AFT T/EDGE FLAP HAS ONE AERODYNAMIC SEAL BROKEN OFF / MISSING JUST INBOARD OF #1 FAIRING -- SEE PHOTO REQUEST DEFERRAL CDL APPLIED -- SHEETMETAL ASST REQD TO REPLACE SEAL WITH RIVETS -- PARTS ADDED PER IPC 27-51-22-01 DISPATCH DESK: 7 SDR SWAA2022032076130Flap · delaminatedL/H O/B AFT FLAP LOWER SURFACE I/B EDGE HAS A DELAM AREA OF APPROX. 14'X14'. MPN:113A3700-25 SN: 004021 / [01] OK TO INSTALL FLAP;[02] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22;[03] INSPECTED WORK PERFORMED ON C/A # 2;[04] 2. SAMUEL SMITH (TECHNICSDR DALA2022040802443None · noneSHIP 3225 CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: R/R STRUT PER A320 AMM 27-51-44. OK FOR SERVICE. (2128517)SDR DALA2022040802440None · noneSHIP 3225 CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING. CORRECTIVE ACTION: R/R STRUT PER A320 AMM 27-51-44. OK FOR SERVICE. (2128534)SDR DALA2022031001550None · noneRT WING UPPER TRAILING EDGE PANEL DAMAGED FWD OF THE OUTBRD SPOILER OUTBRD HINGE. REMOVED DAMAGED "T" AND WEB ASSY FROM AFT WING SPAR. REPLACED THE "T" AND WEB ASSY PER LONG BEACH DWG 9957465, 975008, AND 57-51-09 BOEING 717 SRM. RIB INSTALLATION INSP: QC5312.SDR AALA202202232210Nut · stuckAIRCRAFT IN BASE MAINTENANCE: LEFT WING INTERCONNECTING STRUT NUT SPANNER STUCK. REPLACED INTERCONNECTING STRUT PER TASK CARD 26C57057001.SDR DALA2022022201147None · noneSHIP 3268 CORROSION IB FLAP ELECTRICAL RECEPTACLE INTERCONNECTING STRUT (7540VC) ON RH WING. CORRECTIVE ACTION: REPLACED IB FLAP ELECTRICAL RECEPTABLE INTERCONNECTING STRUT (7540VC) ON RH WING AS PER A320 AWM 27-51-11. OK FOR SERVICE. (2128022)SDR SWAA2022030875181Plate · crackedL/W RSS 261 LOWER REAR SPAR CORRIGATED PLATE IS CRACKED. / [01] REMOVED AND REPLACED L/W RSS 261 LOWER REAR SPAR CORRUGATED PLATE IAW SRM 51-40-02.;[02] VERIFIED REMOVED AND REPLACED L/W RSS 261 LOWER REAR SPAR CORRUGATED PLATE IAW SRM 51-40-02.SDR SWAA2022030875279Panel · delaminatedPANEL 661AB HAS DISBOND SKIN ON OUTER SURFACE / [01] IDENTIFIED PANEL MATERIAL IAW SRM 57-51-01-0I-1 FIG. 3; TABLE 3; ITEM 5. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). <BR><BR>DAMAGE WILL BE REPAIRED ACCORDING TO SDR DALA2022022201179None · noneSHIP 3360 EROSION FLAP TRACK FAIRING 533CB FWD LOWER EDGE ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 597174-14. (2126728)SDR SWAA2022022275111Flap · crackedLH INBD AFT FLAP HAS A DENT ITCH A CRACK ON LOWER SKIN MEASURING 1.0 LENGTH; 0.75 WIDTH; DEPTH .140 AT LOCATION 5.5 FROM TRAILING EDGE AND 20 FROM INBD EDGE CORRECTION IN FAULT: WITH NOT ITCH OUT OF LIMIT PER SRM 57-53-01-1A-2 / [01] PERFORMED TIME-LIMITED REPSDR DALA2022021801107None · noneSHIP 189 FOUND ON WALK AROUND 2 DENTS RT AFT INBD T/E FLAP, CORRECTIVE ACTION: PERMANENT REPAIR COMPLETE PER B767 SRM 57-53-01 (8843888)SDR SWAA2022032173499Fairing · crackedR/H FLAP TRACK # 6 MID FAIRING AREA CRACKED AT INTERNAL SKIN MKD DOT / [01] MESUREMENT;[02] CLEANED AND PREPARED AREA FOR REPAIR; FOUND NO CORE DAMAGE AND NO WATER DETECTED AS PER BOEING 737 SRM51-70-04-2R-1 REPAIR 1.;[03] MEASUREMENT;[04] VERIFIED STEP 1;2; ASDR SWAA2022030773465Bracket · crackedFIXED LH UPPER TRAILING EDGE PANEL 551GB INTERCOSTAL; OB ATTACH L BRACKET IS CRACKED. / [01] REMOVED BRACKET FROM TRAILING EDGE PANEL 551GB PER SRM 51-40-04.;[02] REMOVED AND REPLACED LEFT TRAILING EDGE PANEL 551GB OUTBOARD BRACKET IAW SRM 51-40-02.SDR SWAA2022030176353Flap · delaminatedLH O/B AFT FLAP INBD CORNER HAS EVIDENCE OF DELAM / [01] EVALUATED L/H O/B AFT FLAP INBD CORNER. FOUND AREA OF LESS THAN .50' IN DEPTH & 1.250' IN LENGTH DELAMINATION. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-53-01-2R-4 PAR1A & 3B REV 75. CLEAN AND PREP ARESDR SWAA2022032872759None · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SKIN AT RT WING. 2022-98214 / [01] TOOL USED= CALIPER P/N: 500-197-30; S/N: A21043164; DUE DATE: 01-SEP-22;[02] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 29 SEP 22;[03] TOOL USED FLAW DETSDR DALA2022021500980None · noneSHIP 3268 CORROSION FLAP INTERCONNECT STRUT INTERNAL STRUCTURE ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT RH PER DELTA WORK CARDS AMDS 2750-6010-RT AND 2750-6020-RT. (2121723)SDR DALA2022021500979None · noneSHIP 3268 CORROSION FLAP INTERCONNECT STRUT INTERNAL STRUCTURE ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT LH PER DELTA WORK CARD AMDS 2750-6020-LT AND 2750-6010-LT. (2121719)SDR AALA202202157361Flap · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUT BOARD TRAILING EDGE FLAP UPPER SURFACE HAS DELAMINATION / DISBOND BETWEEN RIB 4 AND RIB 5 IN TRAILING EDGE ZONE 2. REPAIRED FLAP PER SRM 57-53-00-300-100.SDR DALA2022021500983None · noneSHIP 3219 LT WING OB FLAP DENT IN UPPER SURFACE. CORRECTIVE ACTION: REPAIRED PER ERA 597124-14 REV ORIGINAL. OK FOR SERVICE. (2120736)SDR SWAA2022021671814Flap · delaminatedON WALK AROUND FOUND R/H; OUTBOARD; AFT FLAP; LOWER SKIN DELAMINATED. / [01] ADDED EA 22-157-00450 TO FAULT.;[02] REMOVED R/H OUTBOARD AFT FLAP PER AMM 27-51-22;[03] INSTALLED R/H OUTBOARD AFT FLAP UP TO STEP 3F(5)G;[04] INSTALLED R/H OUTBOARD AFT FLAP PER AMMSDR SWAA2022030871566Panel · crackedPANEL 642BB CRACKED ON FWD EDGE SOLID LAMINATE AREA / [01] IDENTIFIED MATERIAL OF PANEL 642BB IAW SRM 57-53-70-0I-3 FIGURE 1-2; 4 AND 7; ITEM #1; TABLE 3 AND 6<BR><BR>BLENDED L/E GOUGE AREA TO .3' X .7'; BLEND EXCEEDS MAXIMUM X MEASUREMENT OF 0.10'; BLEND IS OSDR SWAA2022022871562None · crackedFOUND CRACK ON RT WING O/B AFT FLAP LOWER SURFACE AT 43' FROM O/B EDGE AND 7.5' FROM T/E. PERFORMED VISUAL INSPECTION AND TAP TEST NO DELAMINATION AROUND THE CRACK SIZE 1/2'' IAW NTM 51-05-01 & TOP DRILLED END OF CRACK IAW SRM 51-10-02-0G-0 PARAGRAPH 12.A. SDR DALA2022021500981None · noneSHIP 3255 CREW REPORTS LEFT BELLY FAIRING SLIDING PANEL MISSING ON PRE FLIGHT. CORRECTIVE ACTION: MISSING PANEL CURRENTLY ON CDL. WILL REQUIRE STK 32-5300-3-1439 REF IPC 53-35-03-36 ITEM 70 (8282396)SDR SWAA2022031070032Beam · elongatedELONGATED HOLE ON BEAM LOCATED UPPER INBOARD FIXED TRAILING EDGE RIGHT WING 2022-55831 / [01] REPLACED BEAM LOCATED UPPER INBOARD FIXED TRAILING EDGE RIGHT WING IAW B737-700 DWG 115A2516 SHEET 5 REV- AND SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELLOW.;[02] REPLACSDR SWAA2022030870490Plate · crackedR/W RSS 261 LOWER REAR SPAR CORRIGATED PLATE IS CRACKED. / [01] REMOVED AND REPLACED R/W RSS 261 LOWER REAR SPAR CORRUGATED PLATE IAW SRM 51-40-02.;[02] UPDATED CARD.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2SDR SWAA2022030870492Plate · crackedR/W T/E RSS 271 LOWER SPAR CORRIGATED PLATE IS CRACKED. / [01] REMOVED AND REPLACED R/W T/E RSS 271 LOWER SPAR CORRIGATED PLATE IAW SRM 51-40-02.;[02] UPDATE CARD.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2SDR AALA202202233858Fitting · wornAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING INTERCONNECTING STRUT INBOARD FLAP ON RIGHT WING AND FOUND BORE OUT OF TOLERANCE. ON FITTING ON THE REAR SPAR AT WX4476.559 AND RIB 14. REPLACED FITTING PER SRM 51-42-11.SDR DALA2022042002781Vane · unknownPD: DENTED AND WAS ALREADY ON MONITOR 2170368 FOR OTHER DENTS / CA: REPAIRED PER OEM CMM 27-50-1, REV. 61 WITH APPLICABLE DELTA SUPPLEMENTAL INFORMATION AND CSVE, REV. 30. & ERA'S 598407-14 REV ORIG. AND 598102-14 REV ORIG. / ****LIMITED RELEASE: CMM 27-50-1 FSDR SWAA2022031070031Panel · elongatedELONGATED HOLE ACCESS PANEL 651DT TRAILING EDGE AT RT WING 2022-55824 / [01] TOOL USED CALIPER P/N:500-197-30 S/N:A18234364 DUE DATE:25-SEP-22;[02] TOOL USED: SCALE P/N: CL5000 S/N: AE-408751 DUE DATE: 19-MAR-22;[03] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 15SDR SWAA000069925Panel · pulledPANEL 561BB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). <BR><BR>DAMAGE WILL BE REPAIRED ACCORDING TO SRM 51-70-04-2R-9; AS REQUIRED BY SRM 57-51-01-2R-1; PARA. 4.B.(2); TABLE 202SDR SWAA2022030869924Panel · pulledPANEL 561AB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / REMOVED FINISH & STARTED DAMAGE EVALUATION IAW SRM 57-51-01-1A-1 PARA 2 A (1);[02] DAMAGED FASTENER HOLES ALONG THE MARKED EDGE BAND EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-01-1A-1<BR>PARA 4 B SDR SWAA2022042798251Skin · delaminatedR/H OTBD AFT FLAP INBD LOWER SIDE DELAMED / [01] OK TO INSTALL R/T OUTBRD FLAP AFT FLAP.;[02] OK TO INSTALL R/H O/B AFT FLAP;[03] C/W INSPECTION.;[04] R/R RH O/B AFT FLAP PER AMM 27-51-22;[05] C/W INSPECTION.SDR AALA202203019735Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP INTERCONNECTING STRUT FITTING BEARING HAS EXCESSIVE PLAY, FOUND BORE OUT OF TOLERANCE. REPLACED FITTING PER SRM 51-42-11.SDR IPXA2022021478949Support Angle · noneINSPECTION TYPE:1CLT WING O/B FLAP PANEL T/ESUPPORT ANGLE CRACK AT I/B HINGE.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW DWG # ARC2149 AND SRM 51-31-01,51-35-01 (MINOR).SDR SWAA2022020766961Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP. THE INBOARD CORNER SKIN IS DELAMINATED. THE DELAMINATION IS ON THE AFT SIDE AND MEASURES 2 INCHES BY 4 INCHES. ; / [01] C/W EA # 22-157-00343SDR SWAA2022031066746Panel · brokenBROKEN ACCESS PANEL 551AT TRAILING EDGE INSERT LT WING (1 EA) 2022-55670 / [01] TOOL USED: SCALE P/N: CL5000 S/N: AE-409558 DUE DATE: 19-MAY-22;[02] TOOL USED: HOT BONDER P/N: HCS9200B SN: 18175478 DUE DATE: 05/AUG/22.;[03] REPLACED INSERT (1 E/A) ON ACCESS PA
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