Boeing 737-3S3

Service difficulty reports · 1,209

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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 aircraft_model_key = '7373S3'
  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 AWXA200400867Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP WAS FOUND DELAMINATED AT WBL 262.0, JUST ABOVE NR 2 FLAP FAIRING. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP AT WBL 262.0; CLEANED AND Jul 20, 2004 · N316AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200400777Indicator · faultyON TAKEOFF, EN ROUTE, CAPTAINS AIRSPEED INDICATOR WAS INOPERATIVE, REJECTED TAKEOFF AT 80 KTS AND RETURNED TO GATE. MX ISSUED MEL 34-24, COND 1 (CAPT A/S INDICATOR INOP). WHEN ACFT ARRIVED MX R / R CAPTAINS AIRSPEED INDICATOR IAW BMM 34-12-21. TEARDOWN REPORJul 15, 2004 · N316AW · Boeing 7373S3 · Airspeed/Mach IndicatorSDR AWXA200400800Stringer Clip · crackedDURING C-12 CHECK A .3750 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT STRINGER TIE AT BS 927, STR 24 LT. MAINTENANCE REMOVED AND REPLACED CORRODED STRINGER TIE AT BS 927, STR 24 LT IAW B737-300 SRM 51-40-02.Jul 3, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR AWXA200400799Splice · corrodedDURING C-12 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER SPLICE AT BS 907, STR 25 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AT BS 907, STR 25 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW DWG 65-51698.Jul 2, 2004 · N312AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400804Skin · corrodedMAJOR REPAIR, DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON EXTERIOR FUSELAGE SKIN BELOW CENTER FUEL TANK AT BS 590, LBL 57. MAINTENANCE BLENDED OUT CORROSION ON SKIN BELOW CENTER FUEL TANK AT BS 590, LBL 57, MATERIAL LOSS OUT OF LIMITS; FABRICATED WASHJun 30, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400708Skin · crackedMAJOR REPAIR-DURING C-04 CHECK HFEC INSPECTION OF LOG ITEM DENT, CRACK INDICATION NOTED ON FUSELAGE SKIN AT BS 937,3 INCH ABOVE S24R, APPROX 0.75 INCH LONG. MAINTENANCE INSTALLED A DOUBLER/TRIPLER REPAIR IAW SRM 53-00-01-3 FIG 229.Jun 28, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400792Crease Beam · corrodedLCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR CREASE BEAM (INNER CHORD) BETWEEN BS 950 TO BS 986. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 950 TO BS 986; FABRICATED A NEW REPLACEMENT CREASE BEAM; INSTALLED REPAIRJun 24, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, StructureSDR AWXA200400791Crease Beam · corrodedLCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-2 DOOR CREASE BEAM (INNER CHORD) AT BS 986. MAINTENANCE REMOVED CORRODED CREASE BEAM AT BS 986; FABRICATED A NEW REPLACEMENT CREASE BEAM PER DWG 65-5287697; INSTALLED REPAIR PART IAJun 24, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, StructureSDR AWXA200400796Shear Tie · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE AT BS 500A, STR 16 LT. MAINTENANCE REMOVED CRACKED STRINGER SHEAR TIE AT BS 500A, STR 16 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35350; INSTALLED REPAIR PARJun 23, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, StructureSDR AWXA200400795Shear Tie · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE AT BS 275, STR 15 RT. MAINTENANCE REMOVED CRACKED STRINGER SHEAR TIE AT BS 275, STR 15 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35352; INSTALLED REPAIR PART Jun 23, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, StructureSDR AWXA200400794Skin · corrodedLCQ - MAJOR REPAIR - DURING C-12 CHECK 5 EACH RIVETS WERE FOUND PULLING THROUGH FUSELAGE SKIN AT BS 947, STR 22 LT. MAINTENANCE REMOVED FUSELAGE SKIN FROM BS 907 TO BS 1016, STR 22 LT. FOUND CORRODED INNER DOUBLER AT BS 947, STR 22 LT, REMOVED INNER DOUBLER;Jun 23, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400793Web · corrodedLCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND NUMEROUS FASTENER HOLES ON FORWARD CARGO COMPARTMENT LOWER DOOR SILL WEB BETWEEN BS 440 TO BS 480. MAINTENANCE REMOVED CORRODED LOWER DOOR SILL WEB FROM BS 440 TO BS 480; FABRICATED A NEJun 22, 2004 · N312AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400805Support Angle · crackedDURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND IN SUPPORT ANGLE UNDER KEELBEAM PANEL 3402 AT BS 616. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE UNDER KEEL BEAM PANEL 3402 AT BS 616; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 69-3725Jun 21, 2004 · N312AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400790Skin · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN LEFT L/E SLAT JUST OUTBOARD OF ENGINE PYLON, STAB STA 55.75. MAINTENANCE CUT OUT CRACK IN LEFT L/E SLAT AT STAB STA 55.75; PERFORMED HFEC INSPECTION OF CUTOUT TO VERJun 20, 2004 · N312AW · Boeing 7373S3 · Leading Edge DevicesSDR AWXA200400759Skin Panel · damagedMAJOR REPAIR, DURING C-17 CHECK FOUND 103 LOOSE RIVETS ON BOTH SIDES OF LOWER KEEL BEAM SKIN PANEL BETWEEN BS 663 AND BS 727. MAINTENANCE REMOVED DAMAGED LOWER KEEL BEAM SKIN PANEL FROM BS 661.75 TO BS 727; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN PANEL; Jun 19, 2004 · N315AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400760Splice · crackedDURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN STRINGER SPLICE AT BS 907, STR 4 LT MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 907, STR 4 LT; FABRICATED A NEW REPLACEMENT SPLICE IAW DWG 65-51698-9; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARAJun 15, 2004 · N315AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400658Skin · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK SEVERAL CRACKS WERE FOUND AT RIVET HOLES ON NR 4 LEADING EDGE SLAT FROM SS 28 RT TO SS 84 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF NR 4 SLAT SKIN FROM SS 28 RT TO SS 84 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLJun 6, 2004 · N314AW · Boeing 7373S3 · Leading Edge DevicesSDR AWXA200400657Skin · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 940, STR 20 LT. MAINTENANCE REMOVED EXISTING REPAIR DOUBLERS AND CUT OUT DAMAGED AREA OF SKIN AT BS 940, STR 20 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS Jun 3, 2004 · N314AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400615Skin · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A .625 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER AFT CORNER OF R-1 DOOR CUTOUT JUST ABOVE SCUFF PLATE, EMANATING FROM EDGE OF CUTOUT EXTENDING THROUGH FASTENER HOLE, BS 294, RBL 65, WL 210. MAINTENANCE CUTOUT DAMAGEMay 30, 2004 · N314AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400464Support Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN SUPPORT ANGLE (CLIP) OF AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE (CLIP) AT AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30; FABRICATED A NEW REPApr 27, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400474Web · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB IN SEVERAL LOCATIONS BETWEEN BS 794.3 AND BS 847, RBL 20. MAINTENANCE REMOVED CORRODED SECTION OF AFT CARGO COMPARTMENT DOOR SILL WEB FROM BS 794.3 TOApr 25, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400466Strap · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (STRAP) BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL STRAP AT BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47957; INSTApr 25, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400456Support Angle · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL SUPPORT ANGLE AT BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL SUPPORT ANGLE, BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT ANGLE PApr 23, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400453Reveal · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON R-1 DOOR CUTOUT UPPER AFT REVEAL AT FASTENER HOLE BS 336, STR 10 RT. MAINTENANCE REMOVED CORRODED R-1 DOOR UPPER AFT REVEAL AT BS 336, STR 10 RT; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAApr 22, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400454Panel · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN NR 5 SLAT OUTBOARD COVE PANEL SKIN AT STAB STA 255.7. MAINTENANCE REMOVED CRACKED NR 5 SLAT OUTBOARD COVE PANEL AT SS 255.7; FABRICATED A NEW REPLACEMENT PANEL PER DWG 65C26602; INSTALLED REPAApr 21, 2004 · N313AW · Boeing 7373S3 · Leading Edge DevicesSDR AWXA200400467Web · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND UNDER FORWARD INBOARD CORNER OF AFT CARGO COMPARTMENT DOOR SILL WEB BS 794, RBL 30. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT BS 794, RBL 30; FABRICATED A NEW REPLApr 20, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400465Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN L-1 DOOR SILL WEB, BS 328, LBL 60. MAINTENANCE REMOVED CRACKED L-1 DOOR SILL WEB AT BS 328, LBL 60; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 5Apr 16, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400450Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B5502.Apr 14, 2004 · N313AW · Boeing 7373S3 · FastenersSDR AWXA200400446Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE LT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 LT. MAINTENANCE REMOVED AND REPLACED L/H VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B55002.Apr 14, 2004 · N313AW · Boeing 7373S3 · FastenersSDR AWXA200400451Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT BS 1085, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT IAW T/C I6B55002.Apr 13, 2004 · N313AW · Boeing 7373S3 · FastenersSDR AWXA200400439Vertical Beam · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL WEB BEAM AT LBL 5.7, WL 176. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRApr 13, 2004 · N313AW · Boeing 7373S3 · Fuselage Main, BulkheadSDR AWXA200400441Intercostal · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND IN UPPER ANGLE OF INTERCOSTAL BETWEEN BS 927 AND BS 947, BL "0". MAINTENANCE REMOVED CRACKED UPPER ANGLE ON INTERCOSTAL FROM BS 927 TO BS 947, BL "0"; FABRICATED A NEW REPLACEMENT UPPER INTERCOSTAL ANApr 12, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400445Bolt · corrodedDURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT BS 1088, WL 258. MAINTENANCE REMOVED AND REPLACED R/H HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT IAW T/C I6C55038.Apr 11, 2004 · N313AW · Boeing 7373S3 · Horizontal Stabilizer, Attach FittingsSDR AWXA200400499Skin · crackedMCN - MAJOR REPAIR, DURING C-17 CHECK A .2500 CRACK WAS FOUND AT FASTENER HOLE IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF R-2 DOOR CUTOUT BS 981.8 TO BS 984.8, WL 198. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINApr 9, 2004 · N313AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400452Skin · bulgedMCN - MAJOR REPAIR - DURING C-17 CHECK THE SKIN WAS FOUND BULGING BETWEEN FASTENERS INSIDE THE FORWARD CARGO COMPARTMENT AT A PREVIOUSLY INSTALLED REPAIR DOUBLER BS 370 TO BS 390, RBL 36. MAINTENANCE REMOVED REPAIR DOUBLER BS 370 TO BS 390, RBL 36 AND FOUND EApr 9, 2004 · N313AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400475Stringer · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 967. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 27 L/H AT BS 967; FABRICATED A 4 EACH ANGLES & SHIMS, 2 EACH CHANNELS, AND A HAT SECTION; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-0Apr 8, 2004 · N313AW · Boeing 7373S3 · Fuselage Main, Longeron/StringerSDR AWXA200400437Floor Support · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN FORWARD CABIN FLOOR SUPPORT ANGLE BETWEEN BS 380 AND BS 400, AT BL "0". MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ANGLE FROM BS 380 TO BS 400, AT BL "0"; FABRICATED A NEW REPLACEMENT FLOOR SUPPApr 8, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400373Skin · crackedA 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AFT OF LEFT WING TO BODY FAIRING BS 727E, STR 23 LEFT. MAINTENANCE CUT OUT DAMAGED SKIN AT BS 727E, STR 23 LEFT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SKIN SECTIONApr 8, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400498Angle · corrodedMCN - MAJOR REPAIR, DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON L-1 DOOR SILL IB STIFFENER ANGLES AT SCREW HOLES BS 328, LBL 60. MAINTENANCE REMOVED 2 EACH CORRODED STIFFENER ANGLES AT BS 328, LBL 60; FABRICATED 2 EACH NEW REPLACEMENT ANGLES IAW DWG 6Apr 6, 2004 · N313AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400482Panel · crackedDURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON NR 6 SPOILER PANEL ABOVE ACTUATOR AT WBL 245 RT. MAINTENANCE REMOVED AND REPLACED NR 5 SPOILER PANEL IAW AMM 27-62-11, FIG. 401, PG. 1-5.Apr 6, 2004 · N313AW · Boeing 7373S3 · SpoilersSDR AWXA200400476Skin · delaminatedDURING C-17 CHECK FOUND THE UPPER NO. 5 SLAT WEDGE DELAMINATED AT SS 147.5. MAINTENANCE REMOVED PREVIOUSLY INSTALLED REPAIR DOUBLERS ON NO. 5 SLAT WEDGE AT SS 147.5; FABRICATED NEW REPLACEMENT DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FIApr 6, 2004 · N313AW · Boeing 7373S3 · Leading Edge DevicesSDR AWXA200400481Panel · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON NO. 5 SPOILER PANEL ALONG LEADING EDGE OF LOWER SEAL BETWEEN WBL 71.24 AND WBL 191 R/H. MAINTENANCE REMOVED AND REPLACED NO. 5 SPOILER PANEL IAW AMM 27-62-12, FIG. 401, PG. 1-5.Apr 5, 2004 · N313AW · Boeing 7373S3 · SpoilersSDR AWXA200400480Seat Track · crackedDURING C-17 CHECK EXFOLIATION CORROSION AND A 1 INCH CRACK WAS FOUND ON SEAT TRACK BS 420 TO BS 425, RBL 45. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 380 TO BS 480, RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG 65-46813; IApr 5, 2004 · N313AW · Boeing 7373S3 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200400443Skin · delaminatedDURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 89.5 INCHES FROM INBOARD END WS 378 TO WS 386. MAINTENANCE REMOVED DELAMINATED PREVIOUS REPAIR ON LT OUTBOARD FORE FLAP FROM WS 378 TO WS 386; FABRICATED A REPAIR DOUBLER; BONDEApr 5, 2004 · N313AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200400442Wedge · delaminatedDURING C-17 CHECK THE UPPER SURFACE OF LT INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 9 INCHES FROM INBOARD END. MAINTENANCE CUTOUT DAMAGED UPPER SKIN AND CORE ON LT INBOARD MID FLAP TRAILING EDGE AT WS 82 LT; FABRICATED A NEW REPLACEMENT CORE AApr 5, 2004 · N313AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200400438Skin · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE L/H OUTBOARD AFT FLAP SEPARATING AT THE AFT INBOARD CORNER WS 230.68. MAINTENANCE PERFORMED A BOND REPAIR IAW B737-300 SRM 51-70-10, FIG. 10.Apr 5, 2004 · N313AW · Boeing 7373S3 · Trailing Edge FlapsSDR AWXA200400374Skin · crackedA 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AFT OF EXTERIOR EMERGENCY EXIT LIGHT BS 727, STR 23 RIGHT. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 727, STR 23 RIGHT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SKIN SECTApr 4, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400274Wire Harness · brokenPHX - EEL - DURING INSPECTION A BROKEN SPLICE WAS FOUND ON WIRE FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 2 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND WIRE HARNESS AT SEAT ROW 2 LT, OPERATIONAL CHECK WAS GOOD.Mar 12, 2004 · N312AW · Boeing 7373S3 · Light System WiringSDR AWXA200400299Skin · crackedPHX - MAJOR REPAIR - DURING 8-DAY CHECK SEVERAL CRACKS WERE FOUND PROGRESSING FROM RIVET HOLES ON LOWER LT EDGE OF NR 2 SLAT, SLAT STA 200. MAINTENANCE CUTOUT DAMAGE ON LOWER LT EDGE OF NR 2 SLAT, AT SLAT STA 200; FABRICATED A FILLER AND DOUBLER; INSTALLED REMar 8, 2004 · N314AW · Boeing 7373S3 · Leading Edge DevicesSDR AWXA200400225Battery · dischargedDEN - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.Feb 25, 2004 · N316AW · Boeing 7373S3 · Emergency Equipment
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