JASC 5750

Service difficulty reports · 1,158

Reports filed under 5750 · Wing, Control Surfaces, 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 = '5750'
  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.

SDR FDEA202203170556Bracket · corrodedRIGHT HAND WING - OUTBOARD FLAP ASSEMBLY INBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. RIGHT HAND WING - OUTBOARD FLAP ASSEMBLY. INBOARD FORWARD HINGE (WING SIDE) PIVOT LUG BORE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP ASSEMBLMar 17, 2022 · N594FE · Doug MD11FSDR FDEA202203170541Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750Mar 17, 2022 · N594FE · Doug MD11FSDR FDEA202203170539Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T0Mar 17, 2022 · N594FE · Doug MD11FSDR FDEA202203170538Bracket · corrodedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT BORE CORROSION. FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND E.A.#1-5750-T03Mar 17, 2022 · N594FE · Doug MD11FSDR FDEA202203150817None · wornLH SPL#2 O/B EDGE WEB CHAFING. ACCOMPLISHED THE REPAIR WITH FILLER AND REPAIR SHIM I.A.W EA NO:6-5750-T0367548 P1, SEQ NO:001119, TITLE:WING -FLIGHT SURFACES- LH SPOILER #2 -WEAR MARK ON OUTBOARD FACE OF FRONT SPAR AT LEVEL OF RIB18 & A300-600F SRM 51-27Mar 15, 2022 · N655FE · Airbus A300*SDR FDEA202203150509None · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB19 STGR2.8 COMPLIED WITH EA 6-5750-T0367417 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 11, 19, 25, 26 - ALI 575306-01-1A. REPAIRED THE RH WING CENTER FLAP RIBMar 15, 2022 · N681FE · Airbus A300*SDR FDEA202203150508None · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB25 STGR2.8, RIB26 STGR2.8 COMPLIED WITH EA 6-5750-T0367417 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 11, 19, 25, 26 - ALI 575306-01-1A. REPAIRED THE RH WINGMar 15, 2022 · N681FE · Airbus A300*SDR FDEA202203150507None · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB11 STGR2.7, RIB 11 STGR2.8 COMPLIED WITH EA 6-5750-T0367417 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 11, 19, 25, 26 - ALI 575306-01-1A. REPAIRED THE RH WINMar 15, 2022 · N681FE · Airbus A300*SDR FDEA202203150506None · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB26 STGR2.7, RIB26 STGR2.8, RIB27 STGR2.8 COMPLIED WITH EA 6-5750-T0367416 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AT STRINGERS 2.7 AND 2.8, RIB27 AT STRIMar 15, 2022 · N681FE · Airbus A300*SDR FDEA202203150510None · noneRH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION . SIZE: 20MM*20MM, DEPTH: 1.35MM. COMPLIED WITH EA 6-5750-T0367302 P1. TITLE: WING - FLIGHT SURFACES - RH 3# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE RH WING #Mar 15, 2022 · N681FE · Airbus A300*SDR IPXA2022031380058None · noneINSPECTION TYPE:N/ALEFT WING FLAP UPPER SKIN GOUGE/ PUNCTURE DAMAGEREPAIRED DAMAGE IAW E.O # A300-5750-83011-BMar 13, 2022 · N136UP · Airbus A300F4622RSDR SWAA2022041983096Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AREA LOCATED ON IRSS 214 AT RT WING 2022-122332 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE AREA LOCATED ON IRSS 214 AT RT WING IAW B737-700 DRW 115A2001 SHEET 30 REV A. AND SRM 51-40-02 SRM 51-10-02 ITEM 9;[02] REPLACEDMar 12, 2022 · N7702A · Boeing 7377BDSDR SWAA2022041983097Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AREA LOCATED ON ORSS 244 AT RT WING 2022-122335 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOC. TRAILING EDGE AREA ON ORSS 244 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-92 ITEM 9 AND DWG:115A2001 SHEET 30 REV: A<BMar 12, 2022 · N7702A · Boeing 7377BDSDR SWAA2022041182274Plate · crackedLEFT WING T/E JUST I/B OF #3 FWD CANOE FAIRING HANGER BRACKET WAFFLE PLATE CRACKED LOWER WING SURFACE. / [01] REMOVED AND REPLACED PLATE PER SRM 51-40-02 AND RESTORED PROTECTIVE FINISH PER AMM 51-21-99.;[02] C/W INSPECTIONMar 11, 2022 · N8314L · Boeing 7378H4SDR SWAA2022041182281Plate · crackedRH WING LOWER REAR SPAR WAFFLE PLATE CRACKED JUST OUTBD OF ACCESS PANEL 651DB / [01] REMOVED CRACKED WAFFLE PLATE R/H WING TO F.O.M.;[02] REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-40-02. RESTORED FINISH PER AMM 51-21-99.;[03] INSPECTED AS REQUIREDMar 11, 2022 · N8314L · Boeing 7378H4SDR SWAA2022041982034Access Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AROUND HOLES LT WING 2022-122071 / [01] TOOL USED SCALE P/N: CL5000 S/N: AE-408758 DUE DATE: 09-FEB-23.;[02] TOOL USED HOTBONDER P/N:HCS9200B-AV S/N: 18185781 DUE DATE: 16-JAN-23.;[03] TOOL USED HOT BONDER P/N:HCS9200B-AVMar 10, 2022 · N7702A · Boeing 7377BDSDR SWAA2022041181971Plate · brokenRT WING WIGGLE PLATE AT ORSS 261 IS BROKEN. / [01] REMOVED AND REPLACED R/H WING WIGGLE PLATE AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA 4.;[02] VERIFIED CORRECTIVE ACTION 1.Mar 9, 2022 · N468WN · Boeing 7377H4SDR SWAA2022031481351Plate · crackedR/H WING LOWER TRAILING EDGE SHELF PANEL; JUST OUTBOARD OF THE #6 FLAP TRACK FAIRING HAS A WAFFLE PLATE CRACKED OUT WITH A MISSING NUT PLATE AT ORSS 263; JUST ABOVE THE #2 PYLON AFT FAIRING. / [01] R/R WAFFLE PANEL REF SRM 51-40-02. INSTALLED ONLY 4 OUT 5 FASTMar 9, 2022 · N412WN · Boeing 737*SDR FDEA202203081491Flap · damagedREPAIR ASSESSMENT: L/H WING O/B FLAP UPPER SKIN STA APROX. XOFH 764 - 773 HAS EXISTING BONDED REPAIR DOUBLER DIM. 9" X 5" DOT 22. 0000356511 : LOGAN, DAVID D - 21-JUN-2022 16:14 PREVIOUSLY INSTALLED REPAIR WAS DONE IN ACCORDANCE WITH SRM 57-50-80, REPAIR 1,Mar 8, 2022 · N649FE · Doug MD11FSDR REXA2022060601012Panel · wornRH FLAP ACCESS PANEL 684ET CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS: 4.0"X.75"X.015" DEEP. REMOVE AND REPLACE PANEL.Mar 8, 2022 · N676CA · Cndair CL6002D24SDR FDEA202203081124Flap · damagedREPAIR ASSESSMENT: R/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 243 HAS EXISTING REPAIR DOUBLER DIM. 4" X 5" DOT 21. REPAIRED PER SRM 57-00-00 FIGURE 205, REF. FEDEX EA 1-5750-T0368054Mar 8, 2022 · N649FE · Doug MD11FSDR FDEA202203081123Flap · damagedREPAIR ASSESSMENT: R/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 147 HAS EXISTING ROUND REPAIR DOUBLER DIM. 4" DOT 20. REPAIRED PER SRM 57-00-00 FIGURE 205. REF. FEDEX EA # 1-5750-T0368054 FOR COMPONENT TRACKING.Mar 8, 2022 · N649FE · Doug MD11FSDR FDEA202203081110Skin · unknownREPAIR ASSESSMENT: L/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 189 HAS EXISTING ROUND REPAIR DOUBLER DIM. 3.5". EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-00-00-2R FIG. 205.Mar 8, 2022 · N649FE · Doug MD11FSDR FDEA202203081108None · noneL/H WING I/B FLAP LOWER SKIN STA APROX. XIFH 183 HAS EXISTING ROUND REPAIR DOUBLER, DIM 3.5". EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-00-00 REPAIR GENERAL, FIG. 205.Mar 8, 2022 · N649FE · Doug MD11FSDR FDEA202203081107Skin · unknownREPAIR ASSESSMENT: L/H WING SLAT #5 EXISTING FLUSH REPAIR STA APROX. XOS 661 - 668 ON THE OUTTER SKIN I/B TOP CORNER. EXISTING MEJOR REPAIR PREVIOSULY INSTALLED PER SRM 57-40-01-2R REPAIR 2, FIG. 201, SHT. 1 - 6.Mar 8, 2022 · N649FE · Doug MD11FSDR FDEA202203081105Skin · unknownREPAIR ASSESSMENT: L/H WING SLAT #4 HAS EXISTING FLUSH REPAIR STA APROX. XOS 652 - 660 ON THE OUTTER SKIN O/B TOP CORNER. (DIM 8" X 18") EXISTING MAJOR REPAIR PREVIOSULY INSTALLED PER SRM 57-40-01-2R REPAIR 2, FIG. 201, SHT. 1 - 6.Mar 8, 2022 · N649FE · Doug MD11FSDR FDEA202203080440Slat · wornRIGHT WING SLAT NO. 8 WITH EROSION IN TRAILING EDGE WEDGE WS. 486.2 RIGHT WING SLAT 8 WEAR IN TRAILING EDGE WEDGE AT OSS 494.35 WAS REPAIRED IAW SRM 51- 70-10-2R REPAIR 4 PAG. 149-163. FIG. 202 AND SRM 57-43-02-2R REPAIR 1 FIG. 201 PAG. 1-2 REV. 82 DEC15/2Mar 8, 2022 · N160FE · Boeing 767300SDR SWAA2022041881138Bracket · elongatedLEFT WING LOWER T/E ACCESS PANEL #551GB HAS 1EACH INNER CENTER FITTING WITH ELONGATED HOLE AND 1EACH FWD BLADE SEAL TORN / [01] REMOVED AND REPLACED WITH NEW SEAL AND BRACKET PER BOEING 737-700 SRM 51-40-02-0G-0;[02] CERTIFIED SEAL AND BRACKET (FITTING) REPLACMar 7, 2022 · N947WN · Boeing 7377H4SDR REXA2022042700693None · chafedL/H WING I/B FLAP VANE CAP 584ET HAS CHAFE DAMAGE - REMOVED CHAFE DAMAGE ON FLAP VANE CAP; FOUND TO BE OUT OF LIMITS, DRILLED NEW PART AND PAINTED IAW CRJ-900 SRM 51-12-00-001-001-A01, 57-52-01-101-001-A01, 51-25-01-001-001-A01 AND 51-40-11-001-001-A01.Mar 5, 2022 · N131EV · Cndair CL6002D24SDR SWAA2022032480318Bracket · crackedBELOW THE FIXED OTBD TRAILING EDGE PANEL INBD OF THE DEFLECTION RIB; THE LOWER BULB SEAL BRACKET HAS A CRACK AT THE OTBD UPPER FASTENERS. / [01] REMOVED BRACKET. REF. SRM. 51-40-02;[02] DRILLED UP NEW BRACKET. REF. SRM. 51-40-05;[03] VERIFIED 2. DAVID YECK (TEMar 5, 2022 · N8307K · Boeing 7378H4SDR SWAA2022030779790Tab · crackedLH WING TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACKED. / [01] ACCOMPLISHED STEP 4A THRU 4R AND STARTED TO INSTALL REPAIR PER SRM REPAIR 57-51-02-2R-3.;[02] ACCOMPLISHED PERMANENT REPAIR REF SRM 57-51-02-2R-3Mar 3, 2022 · N7723E · Boeing 737*SDR YENA2022031600235Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE LOCATED LOWER SKIN RIB10 TO RIB11 ON RH WING (CPCP RELATED 572178-01); PERFORMED PERMANENT REPAIR LOC. ON TRAILING EDGE LOWER SKIN RIB10 TO RIB11 ON RH WING IAW EA#57-0038-22 AND RDAF 80109415/159/2022#A AND EMar 1, 2022 · N516JB · Airbus A320232SDR FDEA202203010377Spoiler · damagedLEFT HAND WING NUMBER 7 SPOILER UPPER SURFACE FOUND ONE HOLE AT WBL 224 . REPAIRED LEFT HAND WING NUMBER 7 SPOILER WBL 224 UPPER SURFACE AS PER B777 SRM 57-70-01-2R FIGURE 201 REPAIR 1 AND E.A NUMBER G-5750-T0367259 P1 TITLE : WINGS - FLIGHT SURFACES - LEMar 1, 2022 · N876FD · Boeing 777FS2SDR SWAA2022032978894Plate · crackedA-061 DOT 005 L/H WING WIGGLE PLATE OUTBD OF SAIL TAIL PHENOLIC CRACKED / [01] REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW WIGGLE PLATE P/N 115A3760Y29 TAG # WN 14076 IAW IPC 57-50-00-17;[03] LOCATED AND DRILL HOLES ON NEW PLATE IAW SRM 51-40-Feb 28, 2022 · N8680C · Boeing 7378H4SDR REXA2022040100507Angle · corrodedPANEL 542AZ SUPPORT ANGLE ON AUXILIARY SPAR IS CORRODED. REMOVED & REPLACED ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01Feb 27, 2022 · N910XJ · Cndair CL6002D24SDR SWAA2022032878264Panel · pulledR/W T/E PANEL 661BB HAS SERVERAL PULLED FASTENER HOLE (MARKED) / DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 TABLE 101; PARA 4.B(5SLURRIED FASTENER HOLES WITH 9390 RESIN LOT# JH1GAA7833; MILLED GLASS FIBERS LOT# 1437038-1 AND SET FOR CURE IAFeb 26, 2022 · N238WN · Boeing 737SDR SWAA2022022877644Plate · shearedRT WING LOWER AFT SHELF PANEL 651GB FWD SUPPORT BRACKET(WIGGLE PLATE) HAS SHEARED FASTENERS. / [01] REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-02Feb 24, 2022 · N221WN · Boeing 737*SDR SWAA2022032175632Panel · elongatedPANEL 553ET HAS ELONGATED HOLE (MARKED) / [01] DRILLED UP AND COUNTERSUNK NEW PANEL IAW SRM 51-40-02.;[02] VERIFIED DRILLED UP AND COUNTERSUNK NEW PANEL IAW SRM 51-40-02.;[03] PAINT PANEL 553ET PER AMM 51-21-00;[04] INSPECTED WORK PERFORMEDFeb 20, 2022 · N8315C · Boeing 7378H4SDR SWAA2022032175618Plate · crackedLEFT WING T/E WAFFLE PLATE I/B OF # 3 FLAP TRANSMISSION IS CRACKED.(FOR PNL 551DB). / [01] REMOVED AND REPLACED LEFT WING T/E WAFFLE PER SRM 51-40-02.;[02] SELECT REFERENCE NOT SELECTED. MUST NOT BE TYPED PER THE POD. I'M UNABLE TO COMPLETE CARD;[03] C/W INSPEFeb 19, 2022 · N8315C · Boeing 7378H4SDR SWAA2022030773128Plate · crackedRT WING WAFFLE PLATE CRACKED I/B OF #6 FLAP TRACK / [01] R & R R/H WING WAFFLE PLATE I/B #6 FLAP TRACK PER SRM 51-40-02.Feb 16, 2022 · N8320J · Boeing 7378H4SDR SWAA2022030773027Plate · crackedLEFT WING JUST INBD OF #3 FLAP TRACK; WAFFLE PLATE CRACKED / [01] REMOVED; AND REPLACED WAFFLE PLATE. REF. SRM. 51-40-02;[02] COMPLETEFeb 15, 2022 · N8320J · Boeing 7378H4SDR SWAA2022022172605Plate · crackedRIGHT WING FIXED TRAILING EDGE PANEL WIGGLE PLATE CRACKED. (O/B #6 CANOE) / [01] REMOVED AND REPLACED RIGHT WING FIXED TRAILING EDGE PANEL WIGGLE PLATE PER SRM 51-40-02Feb 15, 2022 · N725SW · Boeing 737*SDR FDEA202202150299Flap · delaminatedRH WING OUTBOARD FLAP LEADING EDGE SKIN WITH DELAMINATION NEAR FLAP TRACK SUPPORT. RH WING OUTBOARD FLAP LEADING EDGE SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 TABLE 1 SHEET 5 AND SRM 51-70-03-0G PAG. 59 SHEET 1 FIG. 18 REV. 82 DEC15/2021Feb 15, 2022 · N158FE · Boeing 767300SDR FDEA202202150298None · delaminatedRH WING -INBOARD TRAILING EDGE FLAP - MAIN FLAP LEADING EDGE WITH DELAMINATION AT 17 INCHES FROM OUTBOARD EDGE. RH WING INBOARD TRAILING EDGE FLAP, MAIN FLAP LEADING EDGE WAS REPAIRED IAW SRM 57- 53-01-2R REP.1 FIG. 201 PAG. 1-9 AND SRM 51-70-17-0G SHEET 1 Feb 15, 2022 · N158FE · Boeing 767300SDR FDEA202202150297Slat · wornSLAT #8 WEDGE AREA REAR FACE WITH SCRATCH (OSS 431). RH WING SLAT #8 T.E. WEDGE AT OSS 431 WAS REPAIRED IAW B767 SRM 57-43-02-2R REP. 1 PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 97-99, 149, 162 REV. 82 DEC15/2021Feb 15, 2022 · N158FE · Boeing 767300SDR FDEA202202150296Slat · wornLEFT WING SLAT NO 5 TRAILING EDGE/LOWER SKIN WITH WEAR TO 31.5 INCHES FROM OUTBOARD EDGE. LEFT WING SLAT NO 5 T.E. WEDGE AT OSS 500 WAS REPAIRED IAW B767 SRM 57-43-02-2R REP. 1 PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 97-99, 149, 162 REV.82 DEC1Feb 15, 2022 · N158FE · Boeing 767300SDR FDEA202202150295Slat · wornLEFT WING SLAT NO 5 TRAILING EDGE/LOWER SKIN WITH WEAR TO 41 INCHES FROM INBOARD EDGE. LEFT WING SLAT NO 5 T.E. WEDGE AT OSS 430 WAS REPAIRED IAW B767 SRM 57--43-02-2R REP. 1 PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 97-99, 149, 162 REV.82 DECFeb 15, 2022 · N158FE · Boeing 767300SDR FDEA202202130287Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2RFeb 13, 2022 · N575FE · Doug MD11FSDR FDEA202202130286Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2RFeb 13, 2022 · N575FE · Doug MD11FSDR FDEA202202130289Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2RFeb 13, 2022 · N575FE · Doug MD11F
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