JASC 5754

Service difficulty reports · 17,348

Reports filed under 5754 · Leading Edge Devices, newest first.

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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 = '5754'
  ORDER BY difficulty_date DESC"

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SDR 96FDEA01170Lug · corrosionMR 0681 AND NR 039. NR 2 K-FLAP HAS CORROSION AROUND OUTBOARD LUG UPPER BOLT HOLE. ****S/D*** REMOVED CORROSION FROM NR 2 K-FLAP, OUTBOARD LUG UPPER HOLE AND REPAIRED PER FEDEX DRAWING SR 27-57-010, REV B.Jun 25, 1996 · N198FE · Boeing 72722SDR UPS96220502Attach Angle · crackedINSPECTION TYPE: C. LT WING FROM SPAR VERTICAL STIFFENER/RIB ATTACH ANGLE IS CRACKED AT RT SLAT O/B TRACK I/B ROLLER MOUNTING RIB. REMOVED, FABRICATED, AND INSTALLED NEW STIFFENER IAW DWG 65-16200 AND SRM 51-30-2 AND 57-10-3.Jun 22, 1996 · N903UP · Boeing 72751CSDR 96FDEA01164Bonding Jumper · corrodedNRO0684 AND 037, NR 2 K-FLAP HAS CORROSION AROUND I/B BONDING JUMPER UPPER AND LOWER ATTACH POINTS. *S/D* BLENDED CORROSION AND REPAIRED RIB IAW FEDEX SRM 57-50-3 AND FEDEX DRAWING SR 27-57-010 REV B.Jun 21, 1996 · N198FE · Boeing 72722SDR UPS96220530Track · corrodedINSPECTION TYPE SI, NR 4 SLAT TRACKS, BOTH HAVE CORROSION ON FWD ENDS AND BOTH SIDES. REMOVED AND REPLACED SLAT TRACKS IAW OHM 57-51-61.Jun 20, 1996 · N929UP · Boeing 72722CSDR UPS96220528Bullnose · corrodedINSPECTION TYPE SI, BULLNOSE CENTER HINGE LOWER ATTACH POINT ON NR 3 K-FLAP IS CORRODED UNDER BOLT HEAD. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.Jun 20, 1996 · N929UP · Boeing 72722CSDR DL72S961497Stiffener · crackedA 1.5 INCH CRACK WING FRONT SPAR VERTICAL STIFFENER AT NR 3 SLAT INBD TRACK CUTOUT. REPLACED SPAR STIFFENER PER M/M 57-20-21.Jun 20, 1996 · N496DA · Boeing 727232SDR UPS96220491Skin · corrodedINSPECTION TYPE: C. RT WING NR 6 K-FLAP IS CORRODED BEYOND ALLOWABLE LIMITS, L/E STA 286.667. REMOVED CORROSION FOUND BEYOND LIMITS. REPAIR IAW 57-50-03.Jun 18, 1996 · N903UP · Boeing 72751CSDR UPS96220504Attach Rib · crackedINSPECTION TYPE: C. NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED IN THREE PLACES. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 51-40-2 AND SRM 51-30-2.Jun 14, 1996 · N903UP · Boeing 72751CSDR UPS96220498Angle · crackedINSPECTION TYPE: C. LT WING FRONT SPAR VERTICLE STIFFENER/RIB ATTACH ANGLE CRACKED AT NR 3 SLAT I/B TRACK I/B ROLLER MOUNTING RIB. REMOVED AND REPLACED STIFFENER ANGLE IAW DWG 65-16200 AND SRM 57-10-2 AND 51-30-2.Jun 14, 1996 · N903UP · Boeing 72751CSDR UPS96220496Angle · crackedINSPECTION TYPE: C. LT WING FRONT SPAR VERTICAL STIFFENER/RIB ATTACH ANGLE IS CRACKED AT NR 3 SLAT O/B TRACK I/B ROLLER MOUNT RIB. REMOVED AND REPLACED STIFFENER ANGLE IAW SRM 51-10-1 AND 51-30-2.Jun 14, 1996 · N903UP · Boeing 72751CSDR UPS96220495Angle · crackedINSPECTION TYPE: C. LT WING FRONT SPAR VERTICAL STIFFENER L/E RIB ATTACH ANGLE CRACKED AT NR 3 SLAT O/B TRACK O/B ROLLER MOUNT RIB. REMOVED VERTICAL STIFFENER ON NR 3 SLAT TRACK ATTACH ANGLE. REPLACED PER SRM 51-10-1, 51-30-2.Jun 14, 1996 · N903UP · Boeing 72751CSDR DL72W961435Angle · crackedNR 6 SLAT LOWER COVE SKIN ANGLE CRACKED 1.5 INCH INBD OF ACTUATOR. REPAIRED PER M/M 57-54-0.Jun 14, 1996 · N294WA · Boeing 727247SDR DL72P961431Skin · crackedSKIN CRACKED AT UPPER TWO FWD FENCE ATTACH HOLES. REPAIRED PER M/M 57-54-0 FIG 813.Jun 14, 1996 · N8875Z · Boeing 727225SDR DL72P961430Skin · crackedSKIN CRACKED AT LOWER FENCE ATTACH HOLE. REPAIRED SKIN PER M/M 57-54-0 FIG 813.Jun 14, 1996 · N8875Z · Boeing 727225SDR DL72P961428Slat · gougedINNER TAI SKIN GOUGED. REMOVED DAMAGE AND REPAIRED PER M/M 57-54-0 FIG 803A.Jun 14, 1996 · N8875Z · Boeing 727225SDR UPS96220494Stiffeners · crackedINSPECTION TYPE: C. LEFT WING AFT SPAR HOLES WORN IN VERTICLE STIFFENERS AT NR 2 SPOILER ACTUATOR FITTING LOWER ATTACH BOLTS. REMOVED AND REPLACED STIFFENERS IAW SRM 57-10-2 51-10-1, AND 51-30-2.Jun 13, 1996 · N903UP · Boeing 72751CSDR 96FDEA01098Fitting · corrodedNR 5 K-FLAP CENTER HINGE FITTING THAT ATTACHES TO FIXED L/E CORRODED. REMOVED AND REPLACED PER SRM.Jun 11, 1996 · N198FE · Boeing 72722SDR 96FDEA01097Fitting · corrodedNR 1 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED. REMOVED AND REPLACED PER SRM.Jun 11, 1996 · N198FE · Boeing 72722SDR 96FDEA01096Fitting · corrodedNR0376 AND 008, NR 2 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED (C57-562-01). *S/D* REMOVED AND REPLACED NR 2 K-FLAP TO LEADING EDGE MOUNT FITTING FOR THE CENTER HINGE IAW SRM 51-30-2.Jun 11, 1996 · N198FE · Boeing 72722SDR DL72P961393Rib · crackedFOUND LEFT WING SLAT RIB CRACKED AT RADIUS, O/B OF ACTUATOR. REPAIRED PER M/M 57-54-0, FIG 804.Jun 10, 1996 · N8875Z · Boeing 727225SDR MZZA96055Skin · crackedTNN - DURING SERVICE CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON RIGHT WING NR 4 LEADING EDGE FLAP INBOARD CORNER UPPER SKIN. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 57-50-3. HANGAR NON-ROUTINE REPAIR ITEM CARD NR 80Jun 6, 1996 · N622DH · Boeing 727264SDR DHL9672183CSkin · dentedAT C-CHECK, NR 6 SLAT EXTERIOR SKIN AT L/E HAS DENT. CUT OUT DENT AREA, FABRICATED DOUBLER 8 BY 4 AND FILLER 1 BY 4 AND INSTALLED PER SRM 57-30-3.Jun 5, 1996 · N721DH · Boeing 727228SDR DHL96721120Angle · crackedAT C-CHECK, NR 7 SLAT ACTUATOR OUTBD TRUNNION ATTACH ANGLE ON FWD SPAR IS CRACKED. FABRICATED NR 7 SLAT ACTUATOR O/B ATTACH ANGLE AND DOUBLER PER S/B 50-0130. INSTALLED ACTUATOR, DOUBLER AND ATTACH ANGLE PER S/B 57-0130.Jun 5, 1996 · N721DH · Boeing 727228SDR UPS96220431Bonding Jumper · corrodedINSPECTION TYPE SI, NR 4 K-FLAP IS CORRODED AT I/B BONDING JUMPER ATTACH POINT ON RIB. REMOVED CORROSION, REMOVED .085 FROM .170 1 BY 1 AREA OUT OF LIMITS. REMOVED CORRODED AREA, FABRICATED REPAIR PARTS AND INSTALLED RELOCATED JUMPER WIRE TO ANOTHER ATTACH PJun 4, 1996 · N929UP · Boeing 72722CSDR UPS96220417Rib · crackedINSPECTION TYPE SI, 2ND AND 3RD RIB CRACKED ON NR 4 SLAT. REMOVED BOTH 2ND AND 3RD RIB FROM SLAT DRILLED UP NEW RIBS AND INSTALLED IN SLAT PER SRM 51-30-2.May 30, 1996 · N929UP · Boeing 72722CSDR UPS96220412Center Hinge · corrodedINSPECTION TYPE SI, BULLNOSE CENTER HINGE UPPER ATTACH POINT ON NR 3 K-FLAP B-CORRODED UNDER BOLT HEADS. REMOVED K-FLAP AND REPLACED WITH NEW K-FLAP.May 29, 1996 · N929UP · Boeing 72722CSDR DL72W961316Rib · crackedRIB NR 21 CRACKED. REPAIRED PER MM 57-54-0.May 29, 1996 · N2820W · Boeing 727247SDR DL72W961315Skin · crackedSKIN CRACKED AT UPPER FWD BOLT HOLE, FENCE ATTACH POINT. REPAIRED PER MM 57-54-0 FIG 813.May 29, 1996 · N2820W · Boeing 727247SDR CALA9600872Rib · crackedINSPECTION FOUND A 1.25 INCH CRACK AT INBOARD ROOT RIB OF RT WING SLAT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-02, FIGURE 2.May 26, 1996 · N33817 · Doug DC982SDR DL72S961273Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED 1 INCH AT ANTI-ICE TUBE CUTOUT, NR 2 SLAT. REPAIRED PER M/M 57-54-0.May 24, 1996 · N490DA · Boeing 727232SDR DL72L961267Fitting · crackedA .6875 INCH CRACK IN NR 5 SLAT AT ACTUATOR ATTACH FITTING. REPAIRED PER M/M 57-54-0.May 23, 1996 · N513DA · Boeing 727232SDR UPS96220213Bullnose Lugs · corrodedINSPECTION TYPE-C, NR 3 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 3 BULLNOSE IAW 57-51-21.May 21, 1996 · N922UP · Boeing 72731CSDR UPS96220212Hinge Fitting · pittedINSPECTION TYPE-C, R/W NR 4 K-FLAP FIXED L/E CTR HINGE FITTING IS PITTIED. REMOVED AND REPLACED NR 4 K-FLAP CENTER HINGE FITTING IAW OHM 57-51-21.May 21, 1996 · N922UP · Boeing 72731CSDR UPS96220211Bullnose Lugs · corrodedINSPECTION TYPE-C, NR 1 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED BULLNOSE LUGS IAW M/M 27-81-01 AND OHM 57-51-01.May 21, 1996 · N922UP · Boeing 72731CSDR UPS96220210Bullnose Lugs · corrodedINSPECTION TYPE-C, NR 2 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 2 K-FLAP BULLNOSE IAW OHM 57-51-21 AND M/M 27-81-01.May 21, 1996 · N922UP · Boeing 72731CSDR CALA9600684Skin · crackedINSPECTION FOUND A 2.875 INCH CRACK IN NR 1 SLAT LOWER SKIN PANEL. A DOUBLER WAS INSTALLED IAW ECRA 5750-01159.May 20, 1996 · N14342 · Boeing 7373T0SDR DL72W961200Stiffener · crackedFOUND ON A-1 LETTER CHECK, FWD SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-21.May 17, 1996 · N2814W · Boeing 727247SDR ARWR960947Skin · damagedDURING C-CHECK, FOUND RT WING UPPER SURFACE INBOARD SLOT, OUTBOARD TRAILING EDGE, HAS TEMPORARY REPAIR. REMOVED TEMPORARY REPAIR, FABRICATED AND INSTALLED NEW REPAIR IAW DER NR 950082-1046. TREATED AND PRIMED IAW SRM 51-1-8. (X)May 14, 1996 · N8969U · Doug DC862SDR ARWR960356Skin · gougedDURING C-CHECK, FOUND LEFT OUTBOARD FLAP APPROXIMATE STA XW217.875 ICE SHIELD LEADING EDGE FLAP CUT-OUT AREA WITH GOUGES AT UPPER SKIN AREA (FRONT SPAR). REPAIRED AREA IAW DER DWG MHA3052. APPLIED CORROSION X IAW SRM 51-1-8 AND CLOSED L/E PANEL IAW SRM 51-3-May 13, 1996 · N8969U · Doug DC862SDR CA960802005Support Fitting · cracked(CAN) #8 INBOARD AUXILIARY TRACK SUPPORT CASTING FOUND CRACKED. ALL DAMAGED ITEMS REPLACED.May 12, 1996 · Boeing 75723ASDR 96FDEA00956Flap · corrodedCORROSION UNDER NR 5 K-FLAP O/B LOWER BONDING JUMPER UPPER ATTACH POINT WENT BEYOND LIMITS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 57-50-3.May 11, 1996 · N468FE · Boeing 727225SDR DL767961188Skin · dentedTHE NR 1 SLAT, TRAILING EDGE WEDGE WAS FOUND DENTED IN THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767-200 SRM 51-70-10 FIG 9.May 10, 1996 · N110DL · Boeing 767232SDR DL72K961123Angle · crackedNR 3 SLAT INBD STOP PAD ANGLE CRACKED. REPAIRED PER M/M 57-54-0 FIG 812.May 10, 1996 · N413DA · Boeing 727232SDR DL72K961121Angle · crackedSKIN ANGLE CRACKED PAST PREVIOUS ROUT OUT BELOW NR 7 SLAT TAI DUCT. REPAIRED PER M/M 57-54-0 PG 807A.May 10, 1996 · N413DA · Boeing 727232SDR EISA96053Rib · crackedFOUND LEFT WING, NR 4 SLAT INTERNAL 5TH RIB FROM INBOARD END, CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-03. (M)May 9, 1996 · N316NE · Boeing 727223SDR EISA96052Rib · crackedLEFT WING, NR 3 SLAT INTERNAL RIB 7TH FROM INBOARD END CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-2 AND 57-50-03. (M)May 9, 1996 · N316NE · Boeing 727223SDR EISA96051Rib · crackedLEFT WING NR 3 SLAT INTERNAL 14TH RIB FROM INBOARD END CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-03 AND 57-50-03. (M)May 9, 1996 · N316NE · Boeing 727223SDR 96FDEA00932Bonding Jumper · corrosionNR0265 AND 002, NR 6 K-FLAP I/B BONDING JUMPER BETWEEN BULLNOSE AND K-FLAP HAS CORROSION AT BOTH MOUNT POINTS. *S/D* REMOVED AND REPLACED NR 6 K-FLAP ON FEDEX NR0477.May 9, 1996 · N199FE · Boeing 727173CSDR 96FDEA00931Bonding Jumper · corrodedNR0264 AND 001, NR 4 K-FLAP I/B BONDING JUMPER BETWEEN K-FLAP AND BULLNOSE HAS CORROSION ON UPPER MOUNT BRACKET. *S/D* REPAIRED NR 4 K-FLAP I/B BONDING JUMPER UPPER ATTACH POINT IAW FEDEX SRM 57-50-3.May 9, 1996 · N199FE · Boeing 727173CSDR ARWR960712Slot Door · corrodedWHILE PERFORMING C-CHECK, FOUND LEFT WING, INBOARD SLOT DOOR TOPSIDE, HAS EXFOLIATION CORROSION IN AREAS MARKED. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW DOUBLAS AIRCRAFT ROD SKETCH NR 96-04-01-0002, AND SRM 51-1-20D AND INSTALLED SLOT DOOR IAWMay 8, 1996 · N8969U · Doug DC862
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