N464FE, cancelled Oct 12, 2012

Service difficulty reports · 225

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N464FE' AND deregistration_id = 'N464FE-2012-10-12'
  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 FDEA201006182051Line · leakingLOST "A" SYSTEM HYDRAULICS AT FL 250. ENG 1 & 2 FLUID SHUTOFF CLOSED FOR 30 MINUTES WITH ENGINE NR 1 & 2 OPERATING. FOUND SPOILER HYD FLUID RETURN LINE NEAR WING STATION 546.5 BROKEN REPLACED SPOILER RETURN LINE PER SPM. LEAK CK`S NORMAL. SYSTEM A PRESSUJun 18, 2010 · N464FE · Boeing 727225 · Hydraulic System, MainSDR FDEA201004131198Rib · crackedNR 3 SLAT 2ND FROM INBD RIB IS CRACKED AT SLAT STA 128. REMOVED CRACKED RIB, FABRICATED NEW RIB USING 7075-O .032 DIMS 18" X 6", HEAT TREATED TO T6 CONDITION IAW ENG REPORT 2-37153-801 REV A, LOCATED, DRILLED AND INSTALLED RIB IAW SRM 51-30-2, 51-20-1, AND 51Apr 13, 2010 · N464FE · Boeing 727225 · Leading Edge DevicesSDR FDEA201004041077Stringer · damagedAFT PIT STRINGER HAS DOUBLE DRILLED HOLES STA 970 STR 28L REMOVED PREVIOUS REPAIR SPLICE AND PRODUCTION SPLICE, REMOVED DAMAGED STRINGER SECTION, LOCATED AND DRILLED NEW STRINGER SECTION USING BAC1498-145 7075T-6 PO 29057141 DIMS 43.1250" AND INSTALLED NEW STRApr 4, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003301031Skin · gougedUPON REMOVAL OF INTERCOSTAL FOUND GOUGE IN FUSELAGE SKIN FWD OF BS 970 BTWN STR 30 AND STR 29R. REMOVED GOUGE AND CORROSION AND FOUND OUT OF LIMITS, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREAS DIMS 2.3750" X 4", 2 3/8" X 5.3125" AND 1" X 3"Mar 30, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003281121Skin · damagedMAIN CARGO AREA STA 660 BETWEEN STR 3L AND 4L NO EDGE DISTANCE ON FASTENERS. CUT OUT DAMAGED AREA DIMS 3" X 3.4", FABRICATED TRIPLER USING 2024T-3 .100 PO 9009120 DIMS 10 7/8" X 11 3/8", FABRICATED DOUBLER USING 2024T-3 .080 PO 9009327 DIMS 11 5/8" X 13 1/2",Mar 28, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003271026Floorbeam · damagedSTA 1166 FLOORBEAM HAS DOUBLE DRILLED HOLES LBL 25. CUT OUT DAMAGED AREA, FABRICATED NEW UPPER CHORD USING BAC1505-100617 7075T-73 PO 29103139 DIMS 11 5/8" X 2", FABRICATED 2 EACH SUPPORT ANGLES USING BAC1490-2831 7075T-62 PO 9006081 DIMS 11 1/2" X 3" AND BMar 27, 2010 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR FDEA201003271021Skin · damagedRT WING OTBD FORE FLAP, INBD L/E WBL 309 TO WBL 314 HAS 2 DEEP GOUGES FROM CONTACT WITH SPOILER PULLEY BOLTS. GOUGES OUT OF LIMITS IAW SRM 57-50-2 ,CUT OUT 2 DAMAGED AREAS DIMS .5" EACH IAW SRM 57-50-4, FABRICATED DOUBLER REPAIR USING 2024T-3 .050 DIMS 7" XMar 27, 2010 · N464FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA201003261016Structure · corrodedCORROSION ON NOSE WHEEL WELL RT MID-CHORD, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 65-19862-20 PO 20017288 AND INSTALLED IAW SRM 51-30-5, 53-10-1 AND 51-30-2.Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA201003261017Sill · damagedC-2 DOOR CUT-OUT LOWER SILL HAS PILLOWING AT BS 970. REMOVED PREVIOUS REPAIR, REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD IAW SRM 51-30-2, LOCATED AND DRILLED NEW CHORD PN 65-56129Y10 IAW SRM 51-30-5 AND INSTALLED CHORD IAW SRM 51-30-2.Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201003261018Skin · corrodedCORROSION ON SKIN FROM STA 580 TO 600 BETWEEN STR 27L AND 28L. THIS NR WAS INCOPORATED IN REPAIR.Mar 26, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003251010Frame · corrodedC-2 DOOR CUTOUT AFT FRAME BS 990, UPPER FLANGE IS CORRODED WITH EXFOLIATION ON LOWER SURFACE BTWN STR. 26R-25R. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 1.5" X 1", FABRICATED REPAIR ANGLE USING 15-5PH .080 DIMS 28" X 3", 2 FILLERMar 25, 2010 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201003251009Skin · damagedL-1 DOOR LOWER LIGHTNING HOLE INNER SKIN IS DAMAGED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE, DIM .1250" IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO NR 9009253, DIM 1" X 3.2500" IAW SRM 51-40-2 FIG 1 AND 52-10-1, FIG 1Mar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew DoorsSDR FDEA201003251008Skin · crackedL-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN IS CRACKED. ROUTED OUT DAMAGE ON L-1 DOOR INNER SKIN LIGHTNING HOLE DIM .1250" IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO 9009253 DIM 1" X 3.7500" IAW SRM 51-40-2, FIG 1. INSTALLED REPAIRMar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew DoorsSDR FDEA201003251007Skin · crackedL-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN HAS UNREPAIRED CRACK, STOP DRILLED. ROUTED OUT DAMAGE AT L-1 DOOR LOWER LIGHTNING HOLE INNER DOOR SKIN DIM 3/4" X 3/4" IAW SRM 51-10-1 REV 102 FABRICATED REPAIR DOUBLER OUT OF 2024 T3 .040" PO NR 9009253 DIM 2Mar 25, 2010 · N464FE · Boeing 727225 · Passenger/Crew DoorsSDR FDEA201003241218Skin · damagedFASTENERS WITH IMPROPER SPACING STA 440 STR 10L. CUT OUT DAMAGED AREA DIMS 11" X 9.4", FABRICATED 3 FILLERS USING 2024T-3 .063 DIMS 11" X 6.75", 9.75" X 11" AND 17.75" X 4.30", FABRICATED DOUBLER AND TRIPLER USING 2024T-3 .071 AND 2024T-3 .090 DIMS 22.50" X 2Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003240986Skin · damagedC-2 DOOR EXTERIOR SKIN HAS ROUTE OUT GREATER THAN .100" AT FWD LOWER CORNER. CUT OUT DAMAGED AREA DIM 3 1/2" X 1 1/2" ON C-2 DOOR FWD LOWER CORNER OF SKIN IAW SRM 51-10-1 AND 52-00-3 FIG 3 FABRICATED REPAIR DOUBLER FROM 2024 T3 .080" PO 9009327 DIM 21 3/8Mar 24, 2010 · N464FE · Boeing 727225 · Cargo/Baggage DoorsSDR FDEA201003240982Stringer · corrodedFWD PIT- CORROSION AROUND DOME NUT IN STRINGER 27R AT BS 705. CORROSION OUT OF LIMITS, REMOVED DAMAGED STRINGER, FABRICATED FILLER USING BAC1498-144 7075T-6 PO 29067266 DIMS 9" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO 20017112 AND INSTALLEDMar 24, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003241049Shear Tie · corrodedCORROSION ON SHEAR TIE AT STA 720C STR'S 28R AND 27R. CORROSION OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3 .040 PO NR 9009253 DIMS 5 INCH BY 2 INCH AND INSTALLED IAW SRM 53-10-1, 53-10-2 AND 51-30-2.Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201003240988Support · crackedCRACK ON SUPPORT ANGLE INSIDE RT ELEVATOR PANEL 9405. REMOVED CRACKED ZEE STIFFENER, FABRICATED NEW ZEE STIFFENER USING 2024T-3 .032 PO NR 9009378 DIMS 18 INCH BY 2.5 INCH, LOCATED, DRILLED AND INSTALLED IAW BOEING 727 SERVICE BULLETIN 55-26 AND SRM 51-30-02.Mar 24, 2010 · N464FE · Boeing 727225 · Elevator StructureSDR FDEA201003240985Skin · misrepairedPREVIOUS REPAIR LOCATED AT STA 1223 STR 23R REQUIRES EVALUATION IAW EO 7-5100-7-5005 PH. REPAIR HAS BLIND FASTENERS INSTALLED. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS IAW SRM 53-30-3.Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003240977Shear Tie · corrodedFWD PIT- CORROSION ON SHEAR TIE AT BS 720, AFT SIDE, BETWEEN STRINGERS 28R AND 28L. CORRSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3 .040 PO 9009253 DIMS 11" X 2" AND INSTALLED IAW SRM 51-30-2, 53-10-2 AND 51- 10-6.Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201003240987Web · crackedFWD CARGO CUTOUT, STA 620, BETWEEN STR 24R AND 25R, CRACKED WEB. CUT OUT DAMAGED SECTION OF WEB, FABRICATED NEW FILLER USING 7075T-6 .071 PO 9009353 DIMS 6" X 4", FABRICATED 2 EACH DOUBLERS USING 7075T-6 .080 PO 9008389 DIMS 4" X 4" AND 4" X 3" AND INSTALLED Mar 24, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201003230981Stringer · corrodedFWD PIT BS 740 STR 27R IS CORRODED AT AFT END. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10", FABRICATED SHIMS USING 20Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003230983Shear Tie · corrodedFWD PIT- CORROSION ON SHEAR TIE AT BS 720A (FWD SIDE) BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE, FWD SIDE BS 720A BETWEEN STRINGERS 28L AND 27L. ORIGINAL THICKNESS .063" MATERIAL LOSS .017" MATERIAL REMAINING .046" FOUND OUT OF LIMITS Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201003230984Shear Tie · corrodedFWD PIT- CORROSION ON SHEAR TIE AT BS 720B, BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE BS 720B BETWEEN STR 28L AND 27L. ORIGINAL THICKNESS .063", MATERIAL LOSS .008" MATERIAL REMAINING .055" FOUND OUT OF LIMITS IAW SRM 51-10-6 AND SRM 53-Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201003230966Stringer · corrodedFWD PIT STA 564 STRINGER 26L CORRODED. CUT OUT DAMAGED STRINGER DIMS 19" X 3" IAW SRM 53-10-3, FABRICATED FILLER USING BAC1498-140 7075T-6 PO 2910023 DIMS 19" X 3" IAW SRM 53-10-3. FABRICATED 2 EACH SPLICES USING BAC1498-132 7075T-6 PO 29067380 DIMS 14"Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003230972Shear Tie · corrodedFWD PIT - CORROSION ON SHEAR TIE AT BS 720A, FWD SIDE, BETWEEN STRINGERS 26R AND 25R. CORROSION OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE USING BAC1505-100155 7075 PO NR 20013256 AND INSTALLED IAW SRM 53-10-1, 53-10-2 AND 51-30-02.Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201003230969Web · gougedMCD CUTOUT INNER WEB IS GOUGED IN SEVERAL SPOTS FROM BS 620 - 640 BTWN STR 4L-5L. REMOVED INNER SKIN AND 2 EACH SPLICER TO MAIN CARGO DOOR AFT UPPER AREA IAW SRM 51-30-2. FABRICATED NEW INNER SKIN MATERIAL USED 2024 T3 .125" DIM. 80" X 48" IAW SRM 53-10-Mar 23, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201003230967Shear Tie · corrodedFWD PIT - CORROSION ON SHEAR TIE AT BS 585, BETWEEN STRINGERS 27R AND 26R - MARKED. REMOVED FRAME TO BS 585 BETWEEN STR 27R AND 26R IAW SRM 51-30-2 FABRICATED NEW FRAME MATERIAL USED 7075 - 0 .063" PO NR 9009527 DIM 10" X 6.5" IAW SRM 51-20-1, FIG 7 ANDMar 23, 2010 · N464FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201003220980Stringer · corrodedFWD PIT- STRINGER 26R IS CORRODED AT BS 740. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8 1/2" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10 1/4", FABRICATED SHIMS USMar 22, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003210970Angle · crackedLT WING T/E FALSE SPAR CHORD ANGLE CRACKED WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB SECTION USING 7075T-6 .032 PO NR 9009201 DIMS 12 1/8 INCH BY 9 1/2 INCH, FABRICATED NEW LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO NR 2911884, FABRICATED 2 ANMar 21, 2010 · N464FE · Boeing 727225 · Wing Miscellaneous StructureSDR FDEA201003201152Skin · damagedFASTENERS WITH IMPROPER SPACING STA 440, STRINGER 19L. CUT OUT DAMAGED AREA, HFEC INSPECTED CUT OUT AND EXISTING HOLES WITH NO DEFECTS NOTED IAW NDTM 51-00-00. FABRICATED REPAIR STRAP USING 2024T-3 .063 PO NR 9009353 DIMS 12 .5" X 4.2500", REPAIR DOUBLER USIMar 20, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003201025Flange · corrodedSURFACE CORROSION ON FUSELAGE STRUCTURE FLANGE AND MONTING BRACKETS FOR FUSELAGE PANEL AFT OF NWW STA 351. CORROSION OUT OF LIMITS, REMOVED, LOCATED AND DRILLED AND INSTALLED NEW CHORD PART NUMBER 65-19861-8 PO# 79014451 IAW SRM 51-30-02 AND 51-30-5.Mar 20, 2010 · N464FE · Boeing 727225 · Fuselage Main, Attach FittingsSDR FDEA201003201024Structure · corrodedAFT CARGO BS 950 LOWER CHORD ANGLE IS CORRODED WITH EXFOLIATION BTWN STR 29L- STR 28L. CORROSION OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PART NUMBER 65-16338-11 PO 20017118 AND INSTALLED IAW SRM 53-10-1, 51-30-5 AND 51-30-2.Mar 20, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201003200979Angle · corrodedFWD PIT- 740 BULKHEAD LOWER CHORD ANGLE IS CORRODED BETWEEN STRINGERS 28R AND 27R. REMOVED DAMAGED ANGLE SUPPORT IAW SRM 51-30-2, FABRICATED ANGLE SUPPORT USING 7075-O .190 DIMS 10.7" X 12" IAW DWG 69-64841, HEAT TREATED TO T6 CONDITION IAW FASI ENG REPORT 2-Mar 20, 2010 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA201003191191Skin · misrepairedFASTENERS WITH IMPROPER SPACING FWD PIT STA 540, STR 27L CUT OUT DAMAGED AREA THRU SKIN MCD STA 540 STR 27L IAW SRM 53-30-3, FIG 1B FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3 FIG 1B CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4, FIG 15 FABRMar 19, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003190963Stringer · corrodedAFT PIT- CORROSION IN STRINGER 27L FROM BS 1005 TO 1010.Mar 19, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003190935Seat Track · corrodedSEAT TRACK CORRODED BS 1142-1165 BL0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION USING 7075T6510, DIMS 44.7500 INCHES LONG IAW P-F SRM 53-10-2 AND INSTALLED IAW SRM 51-30-2.Mar 19, 2010 · N464FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180881Skin · crackedLT OTBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 348 AREA, CUTOUT, SKIN FWD OF FITTING CRACKED. TRIMMED OUT DAMAGED AREA (DIM: .2500"X.2500") IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3, .063", PO NR 9009353, DIM: 6"X4" IAW SRM 57-50-2, FIG 4. TREATEMar 18, 2010 · N464FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA201003180960Structure · crackedAFT A/S LOWER TORQUE BOX LIGHTENING HOLE CRACKED LT SIDE BS 1326.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201003180902Angle · crackedNR 7 SLAT LOWER T/E CHORD ANGLE REPAIR DOUBLER AT INBD UPSTOP PAD IS CRACKED. REMOVED NR 7 SLAT T/E CHORD IAW SRM 57-30-2. LOCATED AND DRILLED NEW T/E CHORD. BAC 1514-1559-2024 T3511 PO 2001728 DIM. 113.7500" IN LENGTH IAW SRM 57-30-5 AND 57-50-2, FIG 2. INSMar 18, 2010 · N464FE · Boeing 727225 · Leading Edge DevicesSDR FDEA201003180928Skin · misrepairedPREVIOUS REPAIR LOCATED AT STA 390 STR 25L REQUIRES EVALUATION IAW EO 7-5100-7-5005 PT1. EVALUATION DETERMINED THE EXISTING REPAIR REQUIRES REPLACEMENT. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER USING 2024T-3 .056, PO 7178367 DIMS 13.5" X 11", FMar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180927Stringer · puncturedFWD CARGO AREA, BS 520, STR 21L, STRINGER HAS PUNCTURE. CUT OUT DAMAGED STRINGER DIMS 14" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6. PO NR 2910023 DIMS 14" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO NR 2001711 DIMS 11" X 3" AND 10" X 3"Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003180926Stringer · damagedFWD CARGO AREA, BS 600, STR 21L, STRINGER HAS DOUBLE DRILLED HOLE. CUT OUT DAMAGED STRINGER DIMS 13" X 3", FABRICATED FILLER USING BAC1498-140 7075T-6 PO NR 2910023 DIMS 13" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO NR 20017112, DIMS 12" X 3" Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA201003180925Tripler · mismanufacturedMCD TRIPLER HAS NUMEROUS FASTENERS WITH IMPROPER SPACING STA 460 STR'S 22L TO 24L. CUT OUT DAMAGED AREAS DIM (13.6250 X 2.7500") AND (2.2500" X 1.7500") IAW PF SRM 53-30-3, FIG 1, CW HFEC INSPECTION IAW B727 NDTM PT 6 51-00-00 FIG 23 & FIG 16, NO CRACKS NOTMar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180921Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD PIT STA 675 STR 25L. CUT OUT DAMAGE AREA THRU SKIN TO STA 675 STR 25L IAW SRM 51-10-1. FABRICATED REPAIR PARTS STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW PF SRM 53-3-3 FIG 1B. CUT OUT DAMAGE SHEAR TIE TO STA 660 STR 27L IMar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180920Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING SKIN FWD PIT STA 600 STR 27L. CUT OUT DAMAGE AREA THRU SKIN STA 600 STR 27L-28L IAW B727 PF 53-30-3 FIG 1B. FABRICATED REPAIR PARTS FILLER, STRUCTURAL FILLER DOUBLER AND TRIPLER IAW PF 53-30-3 FIG 1B. CUT OUT DAMAGE SHEAR TIEMar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180919Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD PIT STA 620 STR 27L. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLER USING 2024T-3 .080 DIMS 89" X 29.5", TRIPLER USING 2024T-3, .125 DIMS 87" X 27.5", 2 STRUCTURAL FILLERS USING 2024T-3 .125 DIMS 90" X 25.5" AND 2024T-3 .Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180918Skin · mismanufacturedFASTENERS WITH IMPROPER SPACING FWD PIT STA 640 STR 27L. CUT OUT DAMAGE AREA TO SKIN STA 640 STR 27L. FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3 FIG 1B CUT OUT DAMAGE SHEAR TIE IAW SRM 53-10-4, FIG 15. FABRICATED SHEAR TIE IAW SRM 53-1Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA201003180917Skin · mismanufacturedFASTENERS WITH ZERO ED FWD PIT STA 680 STR 22L.Mar 18, 2010 · N464FE · Boeing 727225 · Fuselage Main, Plate/Skin
Back to N464FE, cancelled Oct 12, 2012