JASC 5754

Service difficulty reports · 17,344

Reports filed under 5754 · Leading Edge Devices, 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 = '5754'
  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 DHL2006752002Skin · dentedFOUND LEFT WING TEMP REPAIR ON LARGE DENT O/B OF INBD. LANDING LIGHT, BIRD STRIKE. REMOVED AND REPLACED L/W FIXED LEADING EDGE, FROM WS.130 TO WS.349, IAW B727 SRM 51-30-2. OPS CHECKED AND LEAKED CHECKED WING ANTI-ICE SYSTEM, NO LEAKS NOTED IAW B727 MM 30-1Mar 31, 2006 · N752DH · Boeing 727223SDR DHL2006764501Skin · crackedLT WING FIXED LE CRACKED AT NR 4 SLAT OB TRACK CUTOUT, MARKED. REMOVED FASTENERS FOR ACCESS AT LT WING FIXED LE AT NR 4 SLAT OB TRACK CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1, NDT ACCOMPLISHED 727 HMar 30, 2006 · N764AT · Boeing 727264SDR DHL2006764504Structure · crackedLT WING FIXED LE UPPER SURFACE CRACKED AT NR 3 SLAT OB GUIDE (HOOK) CUTOUT AFT OB CORNER, MARKED. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2. STOP DRILLED CRACK IAW B727 SRM 51-10-1, NDT INSPECTED PER 727 PT6 51-00-00 FIG 23 CRACK ENDS IN STOP HOLE. Mar 30, 2006 · N764AT · Boeing 727264SDR DHL2006764508Rib · crackedLT WING INSIDE NR 2 SLAT LE ACTUATOR POINT IB AND OB RIBS HAVE EVIDENCE OF CRACKS, MARKED. HFEC INSP PER 727 PT6 51-00-00 FIG 23 CONFIRMED BOTH RIBS CRACKED. REMOVED AND REPLACED RIB ASSY OB P/N 65-17310-4 PO# 619582 AND IB P/N 65-17310-4 PO# 619577 ON LH WIMar 30, 2006 · N764AT · Boeing 727264SDR DHL2006764507Rib · crackedLT WING INSIDE NR 3 SLAT LE ACTUATOR ATTACH POINT RIB CRACKED, MARKED. REMOVED AND REPLACED INBOARD AND OUTBOARD ATTACH POINT ACTUATOR AT LT WING NR 3 SLAT LE PO NR 6195105 P/N 65-17294-14 AND PO NR 619578 P/N 65-17294-13 IAW B727 SRM 51-30-2.Mar 30, 2006 · N764AT · Boeing 727264SDR ASAA0640315Skin · chafedNR 1 SLAT LOWER TRAILING EDGE SKIN CHAFED. REPAIRED NR 1 SLAT IAW SRM 57 43. 01.Mar 29, 2006 · N784AS · Boeing 7374Q8SDR DHL2006764502Rib · crackedNR 6 SLAT IB ACTUATOR ROD END MOUNT RIB CRACKED. REMOVED AND REPLACED RIB AT NR 6 SLAT IB ACTUATOR ROD MOUNT PO NR 619549 P/N 65-17294-13 IAW B727 SRM 51-30-2.Mar 27, 2006 · N764AT · Boeing 727264SDR DHL2006764514Rib · crackedFOUND CRACK INDICATION ON NR 7 SLAT I/B ACTUATOR ROD END MOUNT RIB. REMOVED AND REPLACED RIB ASSY P/N 65-17310-3 PO NR 619595 AND P/N 65-17310-4 PO NR 61956. CHANNEL P/N 65-17310-7 PO NR 619596 IAW B727 SRM 51-30-5 AT NR 7 SLAT IB AND OB ACTUATOR ROD END MOUMar 27, 2006 · N764AT · Boeing 727264SDR UIEA200600074Seal · crackedNR 11 KRUEGER FOUND WITH FOLLOWING DEFECTS, UPPER STIFFENER FOUND CRACKED AT INBD SIDE. BULLNOSE MICA STRIP MISSING. OUTBD CURVE SEAL EDGE ON FLAP FOUND CRACKED. TORN SEAL AT TOP, AND BOTH SIDES, PN=65B39200-9, SN=000302. REPAIRED CARRIED OUT AS PER SWJC: Mar 27, 2006 · N540MC · Boeing 747243BSDR UIEA200600072Bearing · wornNR 12 KRUEGER FOUND WITH FOLLOWING: 5 OUTBD HINGE BEARING FOUND WORN. SEAL FOUND TORN AT TOP AND BOTH SIDES. REPAIRED CARRIED OUT AS PER SWJC:MSG 61/02/06.Mar 27, 2006 · N540MC · Boeing 747243BSDR 06FDEA1243Structure · damagedCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS BLEND REPAIR 3 EACH ON RT SIDE NR 2 L/E SLAT TRAILING EDGE UNABLE TO DETERMINE APPROVED REPAIR. DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED PEMar 27, 2006 · N426FE · Airbus A310203SDR QXEA200600824Flange · chafedPDX - C4 LOWER MOUNT FLANGE FOR ELADING EDGE PANEL 511AL CHAFED BOTTOM INBOARD END. REPAIRED IAW RD 8-57-1150.Mar 25, 2006 · N354PH · Dhav DHC8202SDR UIEA200600060Beam · crackedLT WING FIXED LEADING EDGE NOSE BEAM CAP LOWER SKIN FOUND CRACKED AROUND FASTENERS AT ILES 630. LHW FIXED LEADING EDGE SKIN AT ILES 630. CRACKED REPAIRED AS PER BOEING MSG 1-166123104-2,FAA FORM 8100-9 DATED 24 MARCH 2006.Mar 25, 2006 · N540MC · Boeing 747243BSDR 06FDEA1204Fastener · corrodedDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: LT WING, DROPPED LEADING EDGE, EXISTING REPAIR DOUBLER ON UPPER SIDE. REMOVED RUST ON FASTENER BY BRUSHING AND REPROTECTED IAW SRM 51-21-01. EXISTING REPAIR IS CONFORM TO SRM 57-10-00 FIG 55 FOLLOWING EOMar 23, 2006 · N568FE · Doug DC1010SDR ASAA0540196Skin · delaminatedRT NR 5 SLAT OB T/E IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)Mar 22, 2006 · N782AS · Boeing 7374Q8SDR UIEA200600050Skin · crackedLT WING LEADING EDGE FIXED BULLNOSE, FOUND CRACKED AT BOTTOM CUT-OUT, AT NR 12 KRUEGER INBD LINKAGE MOUNTING AREA. ILES 445 LOWER BEAM. LHW LOWER BEAM CRACK REPAIRED AS PER BOEING MSG. 1-168482122-2 AND FAA 8100-9 DATED 20 MARCH 2006.Mar 21, 2006 · N540MC · Boeing 747243BSDR UIEA20060052Mount · crackedRHW NR 15 KRUEGER FLAP TOP MOUNTING POINT (O/B) CUT OUT AT LEADING EDGE CAP, FOUND WITH HEARLINE CRACK PROPAGATING FROM FASTENER HOLE (LWR BEAM), ILES 514. RHW LOWER BEAM CRACK REPAIRED AS PER BOEING MSG 1-168482122-2, AND FAA 8100-9 DATED 20 MARCH 2006.Mar 21, 2006 · N540MC · Boeing 747243BSDR TSAA0657024Skin · gougedWING LEADING EDGE SKIN GOUGED AT WBL 340.Mar 21, 2006 · N818AL · Boeing 737230SDR AWXA200600751Skin · delaminatedDURING C12 CHECK DISCOVERED 2 SQUARE INCH AREA OF DELAMINATION ON THE UPPER SURFACE OF THE NR 8 SLAT, TRAILING EDGE WEDGE AT THE INBOARD END AT WBL 440R. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 757-200 SRM 51-70-10-2R. FABRICATED FILLER AND DOUBLER IAW BMar 20, 2006 · N910AW · Boeing 7572G7SDR AWXA200600653Wedge · delaminatedGYR - DURING C12 CHECK DISCOVERED ONE SQUARE INCH DELAMINATION AREA ON TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FROM OB EDGE. MAINTENANCE CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED FABRICATED PARTS TO TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FRMar 20, 2006 · N910AW · Boeing 7572G7SDR DHL2006801503Frame · crackedRT OUTER WING OTBD L/E CRACK 0.500" ON FORMER STA XFS 822.50. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. Mar 20, 2006 · N801DH · Doug DC873FSDR DHL2006801504Frame · crackedRT OUTER WING OTBD L/E CRACK 0.500" ON FORMER STA XFS 791.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLE DOUBLER (AL7075T6 0.040") AND PERFORMED STOP HOLE IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B.Mar 20, 2006 · N801DH · Doug DC873FSDR DHL2006801502Frame · crackedFOUND RT OUTER WING OUTBD L/E FRAME CRACK 0.500" STA 766.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLE DOUBLER (AL 7075T6 0.040") AND PERFORMED STOP HOLE IA SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALMar 20, 2006 · N801DH · Doug DC873FSDR QXEA200600719Structure · chafedYYC - C4 LEFT HAND WING LOWER LEADING EDGE REBATE IS CHAFED AT YW 57.2 AND HAS SEVERAL LOOSE AND MISSING SLEEVES. REPAIRED IAW RD 8-57-3328, ISSUE 2, 8-57-811, ISSUE 3 AND HORIZON AIR EA 2-57-354.Mar 17, 2006 · N350PH · Dhav DHC8202SDR SWAA060876Skin · delaminatedDURING SCHEDULED SPECIAL VISIT, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE DELAMINATED. REPAIRED SLAT PER SRM.Mar 16, 2006 · N315SW · Boeing 7373H4SDR UPS06146492Rib · crackedINSPECTION TYPE:5YR LT WING KRUEGER FLAP AREA CURVED DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER A300 SRM 51-40-00.Mar 15, 2006 · N131UP · Airbus A300F4622RSDR DHL2006750509Skin · gougedNR 6 SLAT TRAILING EDGE IS GOUGED AT OUTBD HOOK. ROUTED OUT GOUGE .200 RADIUS BY 6" AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. FABBED REPAIR DOUBLER FROM 7075 T6 A125 PO5096301 DIM 8 1/2 BY 3 1/2 IAW B727 SRM 57-50-3 FIG10. TREATED AND PRIMEMar 13, 2006 · N750DH · Boeing 7272M7SDR UIEA200600035Skin · erodedLT WING LEADING EDGE VCF PANEL NR 10 UPPER SIDE HAS EROSION DAMAGE. REPAIRED PANEL NR 10 IAW OHM 57-55-22 AND SRM 51-40-14 PARA 4K AND FIG 16.Mar 13, 2006 · N512MC · Boeing 747230BSDR UIEA200600034Panel · erodedLEFT WING LEADING EDGE PANEL VCF NR 6 LOWER SIDE OF PANEL IS EROSION DAMAGE, AND LOWER SIDE CHANNEL IS DAMAGED. REPAIRED VCF NR 6 IAW OHM 57-55-22 AND SRM 51-40-14 PARA 4N AND FIG 16.Mar 13, 2006 · N512MC · Boeing 747230BSDR 06FDEA1015Doubler · crackedLEFT WING L/E CRACK INTERNAL DOUBLER AND SPLICE AT STA XOS 670. REPLACED DOUBLER IAW SRM 51-33-01 PAR 6-10 AND SRM 51-35-01 PAR 1-5 VOL 2 AND IAW DWG 1249, PERFORMED REPAIR DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.Mar 13, 2006 · N68054 · Doug MD1010FSDR 2006UALA00465Wedge · damagedNR 6 SLAT WEDGE HAS A HOLE LOWER SIDE JUST ABOVE ACTUATOR. NR 6 SLAT WEDGE HOLE WAS REPAIRED PER SRM 57-70-11 REPAIR NR 4.Mar 11, 2006 · N928UA · Boeing 737522SDR 2006UALA00464Skin · delaminatedRIGHT WING NR 5 L/E SLAT END UPPER SURFACE DELAMINATED. RT WING NR 5 LE SLAT END UPPER SURFACE DELAMINATION REPAIRED PER SRM 51-70-10.Mar 11, 2006 · N928UA · Boeing 737522SDR TSAA0653017Spar · corrodedCORROSION ON UPPER & LOWER SURFACE OF FRONT SPAR LOWER CORD BETWEEN FSS 297 & FSS-306 AT SLAT NR 4. BLENDED INBOARD - OUTBOARD DIRECTION 10:1 DEPTH TO BLEND RATION. SHOT/FLAP PEEN BLENDED ARE PER SRM. FABRICATED SOLID FILLERS TO REPLACE REMOVED MATERIAL. FMar 11, 2006 · N810AL · Boeing 7372Y5SDR TSAA0627016Slat · bird strikeON CLIMB AT 1000 FT AIRCRAFT STRUCK A LARGE BIRD AT NR 1 LEADING EDGE SLAT. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH FORM M-106 BIRD STRIKE INSPECTION AND FOUND A LARGE DENT APPROXIMATELY 1.5 INCH WIDE ON THE OUTBOARD LEADMar 11, 2006 · N808AL · Boeing 7372T4SDR SWAA060786Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT ASSY PER SRM.Mar 10, 2006 · N630WN · Boeing 7373H4SDR IXXA06SMN074SVane · damagedDURING ROUTINE C CHECK, LT WING L/E INBD SLOT VANE HOLES ELONGATED, XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06, SEMAN DWG ED 4186 DATE 03-04-06, EO SEMAN 2006146 DATE 03-07-06. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM Mar 9, 2006 · N602AL · Doug DC873FSDR SWAA060783Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING L/E SKIN CRACKED AT WS 213. REPAIRED SKIN PER SWA EA.Mar 9, 2006 · N392SW · Boeing 7373H4SDR SWAA060754Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 L/E SLAT INBOARD LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.Mar 8, 2006 · N630WN · Boeing 7373H4SDR SWAA060753Wedge · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND RIGHT WING NR 5 L/E SLAT UPPER T/E WEDGE DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM.Mar 8, 2006 · N514SW · Boeing 7375H4SDR TAMF20060010SSkin · corrodedDURING C CHECK INSPECTION WAS FOUND A CORROSION ON LEADING EDGE SLAT NR 5, STA WS 460.2. / DAMAGE WILL BE REPAIRED IAW EWO 767 57-009 AND MFG SERVICE REQUEST ID 1-171332193. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.Mar 7, 2006 · N767QT · Boeing 767200SDR AWXA200600442Skin · delaminatedGYR - MAJOR REPAIR - DURING C8 CHECK DISCOVERED 4 SQUARE INCH DELAMINATION AREA ON UPPER SURFACE OF THE NR 6 LEADING EDGE SLAT, 8 INCHES FROM THE OUTBOARD EDGE AND 8 INCHES FROM THE TRAILING EDGE, INBOARD OF THE NR 2 ENGINE. MAINTENANCE REPAIRED THE NR 6 SLATMar 7, 2006 · N907AW · Boeing 757225SDR AWXA200600441Skin · delaminatedGYR - DURING C8 CHECK DISCOVERED THE LT LEADING EDGE INBOARD SLAT, INBOARD OF THE NR 1 ENGINE, SHOWS MULTIPLE SIGNS OF DELAMINATION PRESENT. MAINTENANCE REPAIRED THE DELAMINATED AREAS ON LT LEADING EDGE INBOARD SLAT, INBOARD OF THE NR 1 ENGINE, USING RESIN ANMar 7, 2006 · N907AW · Boeing 757225SDR AWXA200600440Skin · delaminatedGYR - DURING C8 CHECK DISCOVERED THE LT LEADING EDGE SLAT AREA AT THE NR 2 SLAT INBOARD LOWER MATING EDGE SHOWS DELAMINATION PRESENT. MAINTENANCE REPAIRED THE DELAMINATED AREA ON THE LT LEADING EDGE SLAT AT THE NR 2 SLAT INBOARD LOWER MATING EDGE USING RESIN Mar 7, 2006 · N907AW · Boeing 757225SDR AWXA200600439Skin · delaminatedGYR - DURING C8 CHECK DISCOVERED THE RT LEADING EDGE SLAT AREA BETWEEN NR 9 AND NR 8 SLAT, THE INBOARD EDGE SHOWS DELAMINATION PRESENT. MAINTENANCE REPAIRED THE DELAMINATED AREA ON THE RT LEADING EDGE SLAT BETWEEN 9 AND 8 USING RESIN AND GLASS IAW BOEING 757-Mar 7, 2006 · N907AW · Boeing 757225SDR AWXA200600438Skin · delaminatedGYR - DURING C8 CHECK DISCOVERED THE RT LEADING EDGE SLAT AREA BETWEEN NR 10 AND NR 9 SLAT, THE INBOARD EDGE SHOWS DELAMINATION PRESENT. MAINTENANCE REPAIRED THE DELAMINATED AREA ON THE RT LEADING EDGE SLAT BETWEEN 10 AND 9 USING RESIN AND GLASS IAW BOEING 75Mar 7, 2006 · N907AW · Boeing 757225SDR SWAA060745Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE DELAMINATED AT INBD END. REPAIRED SLAT PER SRM.Mar 7, 2006 · N630WN · Boeing 7373H4SDR ASAA0640231Structure · damagedNR 6 SLAT CHAFED ON AFT SIDE AT SLAT STA 278. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.Mar 7, 2006 · N705AS · Boeing 737490SDR 2006UALA00399Skin · puncturedNR 1 KRUGER FLAP DAMAGED, PUNCTURED APPROXIMATELY 1.2 BY 100 PERCENT THRU. PERMANENT REPAIR DOUBLER WAS INSTALLED PER AAR EA I060103 SUPPORTED WITH 8100-9 FORM.Mar 4, 2006 · N326UA · Boeing 737322SDR DHL2006760511Rib · crackedLEFT WING NR 3 L/E SLAT ACTUATOR ROD END OUTBOARD ATTACH SHOWS EVIDENCE OF CRACK. REMOVED AND REPLACED O/B RIB AT NR 3 L/E SLAT LEFT WING IAW B727 SRM 51-30-2.Mar 4, 2006 · N760AT · Boeing 7272B7SDR ABXA060165Repair · crackedRIGHT WING LEADING EDGE EXTERIOR TOP SURFACE REPAIR DOUBLER WAS CRACKED JUST INBOARD AND AFT OF OUTBOARD SLOT. REMOVED AND REPLACED DAMAGED EXISTING REPAIR DOUBLER FORM UPPER SKIN TRAILING EDGE SECTION IAW DC8 SRM 57-2-1.Mar 2, 2006 · N828AX · Doug DC863F
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