N465FE, cancelled Aug 10, 2015

Service difficulty reports · 85

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 = 'N465FE' AND deregistration_id = 'N465FE-2015-08-10'
  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 FDEA201203221062Slide · dislodgedEMERGENCY SLIDE CAME OUT OF DOOR WHEN OPENING. DID NOT DEPLOY. INSTALLED EMERGENCY ESCAPE SLIDE IAW MM 25-60-015-2-0.Mar 22, 2012 · N465FE · Boeing 727225 · Escape SlideSDR FDEA201008313206Light · looseEMERGENCY EXIT LIGHT IN COCKPIT POPS OUT OF ITS HOUSING ON ROTATION AND LANDING. FOUND LIGHT NOT PROPERLY SET, RE-SET SAME, OPS CHECK NORMAL AND NOW IS SECURE. ACCOMPLISHED IAW MM 33-50-101-2-0.Aug 31, 2010 · N465FE · Boeing 727225 · Emergency LightingSDR FDEA201008313205Light · damagedCOCKPIT EMERGENCY EXIT LIGHT DOES NOT TEST ON PRE-FLIGHT. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD. Aug 31, 2010 · N465FE · Boeing 727225 · Emergency LightingSDR FDEA200910163595Rib · crackedNR 3 SLAT HAS 2 CRACKED RIBS, INBD AND OTBD OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIBS, FABRICATED NEW RIBS, HEAT TREATED RIBS TO T4 CONDITION IAW FASI FORM 2-37153-801 REV A AND INSTALLED IAW SRM 51-30-2 AND 51-20-1.Oct 16, 2009 · N465FE · Boeing 727225 · Leading Edge DevicesSDR FDEA200910143576Angle · crackedNR 1 SLAT LWR AFT CHORD ANGLE IS CRACKED BELOW ACTUATOR. REMOVED ACCESS PANEL IAW SRM 51-30-2, CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101, FABRICATED NEW LOWER CHORD, AND 1 EACH SPLICER IAW SRM 57-50-2 FIG 2 AND 51-40-4 FIG 1 REV 101, TREATED AND PRIMED Oct 14, 2009 · N465FE · Boeing 727225 · Leading Edge DevicesSDR FDEA200910143588Structure · crackedR/WING INBD MIDFLAP T/E CHORD CRACKED AT NR 2 AFT FLAP HINGE CUTOUT. REMOVED LOWER CHORD SECTION IAW SRM 51-30-2 LOCATED AND DRILLED NEW LOWER CHORD, INSTALLED NEW CHORD IAW SRM 51-30-2 REV 101 INSTALLED LOWER MIDFLAP PANEL IAW SRM 51-30-2 REV 101.Oct 14, 2009 · N465FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA200910133624Shear Tie · corrodedAFT PIT CORROSION AT SHEAR TIE STA 950E STR 29R REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT SHEAR TIE, FABRICATED REPAIR ANGLE USING 7075-0 .080 PO NR 9008557 DIMS 6" X 2", HEAT TREATED ANGLE TO T6 CONDITION IAW FASI FORM 2-37153-801 REV A AND INSTALLEOct 13, 2009 · N465FE · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA200910133553Skin · gougedLT INBD MIDFLAP UPPER SURFACE IS GOUGED WBL 80. MIDFLAP REMOVED AND REPLACED DUE TO DAMAGE BEING OUT OF LIMITS AND BEYOND ECONOMICAL REPAIR.Oct 13, 2009 · N465FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA200910123625Frame · corrodedE AND E COMPARTMENT BS 400 STR 19R CORROSION NEXT TO TOOLING HOLES. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 1" DIAMETER, FABRICATED NEW FRAME REPAIR USING 7075-0 .050 PO NR 29016223, DIMS 9 3/4" X 5 1/2", HEAT TREATED PART TO T6Oct 12, 2009 · N465FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA200910123546Skin · gougedRT OTBD FOREFLAP, GOUGED AND CHAFED AT OTBD L/E. GOUGE OUT OF LIMITS IAW SRM 51-30-2, FABRICATED REPAIR DOUBLER, IAW SRM 57-50-4, FIG 1 REV 101, TREATED AND PRIMED REPAIR DOUBLER IAW SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, REV 101.Oct 12, 2009 · N465FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA200910103545Lap Joint · damagedSTA 620, STR 27L, LAP SEAM LWR ROW, NO DISTANCE BETWEEN RIVETS. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND INSTALLED REPAIR AND FASTENERS IAW SRM 51-30-2, 53-30-3, 51-30-8 AND 51-10-2.Oct 10, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200910093552Floor Support · corrodedL-1 ENTRANCE WALK WAY BS 300-340, LBL 56- RBL 30, FLOOR SUPPORTS LWR SURFACES HAVE CORROSION AT N/P HOLES AS MARKED. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA DIMS 2" X 1", FABRICATED 2 EACH REPAIR ANGLES USING 7075-0 .063 PO 9008655 DOct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910093531Angle · crackedAFT AIRSTAIR RT LOWER TORQUE BOX, UPPER WEB SUPPORT ANGLE IS CRACKED AT STA 1273 ON FWD SIDE RADIUS. REMOVED ANGLE SUPPORT IAW SRM 51-30-2, LOCATED AND DRILLED NEW ANGLE SUPPORT IAW SRM 51-30-5 REV. 101. INSTALLED NEW UPPER WEB SUPPORT ANGLE IAW SRM 51-30-2 Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910093533Vertical Beam · misinstalledFUSELAGE STA 1183 LWR CHORD LT INBD 17.8 VERT BEAM FASTENERS SPACING SHORT. REPAIR ACCOMPLISHED ON NON-ROUTINE N00323 UNDER WORK ORDER 00045711 IAW EA 7-5310-126851.Oct 9, 2009 · N465FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA200910093532Frame · crackedAFT AIRSTAIR RT LWR TORQUE BOX, UPPER WEB SUPPORT ANGLE IS CRACKED AT STA 1263 ON AFT SIDE RADIUS. REMOVED WEB DOUBLER, REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE USING 7075-0 .090 PO 9008486 DIMS 18" X 5 7/8", HEAT TREATED ANGLE TO T6 CONDITION IAW FASI FOct 9, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910083518Skin · corrodedSKIN BULGE STA 1050, STR 27L. FOUND EXFOLIATED CORROSION OUT OF LIMITS ON SKIN, CUT OUT DAMAGED AREA, CUT OUT DAMAGED STRINGER SECTION, FABRICATED REPAIR DOUBLER AND FILLERS, FABRICATED STRINGER REPAIR AND SPLICES, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2, Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200910083519Stringer · damagedMAIN CARGO AREA, STA 450, STR 3L NO EDGE DISTANCE BETWEEN RIVET AND HOLE. REMOVED FASTENERS AND CUT OUT DAMAGED AREA, FABRICATED ONE FILLER, ONE PLATE, TWO PLATES, TWO PLATES AND INSTALLED IAW SRM 51-30-2, 53-10-3 AND 51-10-2.Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200910083517Keelbeam · crackedLT KEELBEAM CHORD IS CRACKED AT BS 870, LBL 4. CUT OUT DAMAGE AREA DIM 2" IAW FEDEX 727 EA 7-5310-135501, FAB REPAIR DOUBLER MAT USED 15-5 PH .071" PO # 290342001 DIM (85/8" X 4") IAW EA 7-5310-135501. ACCOMPLISHED HARDNESS TEST VERIFICATION OF FABRICATEOct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, KeelSDR FDEA200910083516Vertical Beam · damagedAFT CARGO COMPT, BS 1183 PRESSURE BULKHEAD LBL 17.8 VERTICAL BEAM WEB HAS SEVERAL DOUBLE DRILLED HOLES AT WL 190. REPAIR ACCOMPLISHED ON NON-ROUTINE N00323 UNDER WORK ORDER 00045711 IAW EA 7-5310-126851, REFERENCE SDR 09-3493.Oct 8, 2009 · N465FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA200910073499Stringer · corrodedFWD CARGO COMPARTMENT- CORROSION ON STRINGER 27R AT END SPLICE, BS 740. CUT OUT DAMAGE STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED NEW SECTION STRINGER AND 1EA SPLICE IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED STRINGEOct 7, 2009 · N465FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA200910063491Stringer · damagedFORWARD CARGO AREA, STA 580, STR 21L, DRILL START ON STRINGER. CUT OUT DAMAGED AREA DIM 17 5/8" LONG IAW SRM 51-10-3 FIG 1 REV 101, FABRICATED HAT SECTION, AND 2 EACH SPLICERS 2 EACH CHANNELS, 2 EACH ANGLES AND 2 EACH FILLERS IAW SRM 53-10-3 FIG 1 AND 53-1Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FDEA200910063493Angle · crackedNR 7 SLAT AFT LWR CHORD ANGLE IS CRACKED 2 PLACES BELOW T-DUCT. REMOVED ACCESS PANEL IAW B 727 SRM 51-30-2. REMOVED LOWER CHORD ANGLE IAW SRM 51-30-2. FABRICATED A NEW LOWER CHORD AND 1 EA SPLICE IAW SRM 57-50-2 FIG 2, AND 51-40-4 FIG 1. TREATED AND PRIMED IAOct 6, 2009 · N465FE · Boeing 727225 · Leading Edge DevicesSDR FDEA200910063495Skin · damagedDRILL START STA 261 STR 21L. CUT-OUT DAMAGED AREA AND FABRICATED REPAIR FILLER AND DOUBLER IAW B727 SRM 53-30-3 FIGURE 3A. TREATED AND PRIMED PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS AT BS 261 STRINGER 21LT IAW SRM 53-30-3 FIGURE 3A.Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200910063490Web · crackedSTA. 1323, STR 20, LEFT AFT AIRSTAIR EQUIPMENT AREA, CRACK ON WEB. TRIMMED AREA IAW SRM 51-10-1 REV 101 FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 5 REV 101 AND SRM 53-10-2 FIG 6 TREATED AND PRIMED IAW 51-10-2 REV 101 INSTALLED DOUBLER AT STA 1323 STR 2Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200910063492Skin · crackedNR 7 SLAT INBD HOOK AFT MOUNTING FASTENER IS LOOSE AND EDGE OF COUNTERSINK HAS CRACK INDICATION. HFEC INSPECTED AREA IAW NDTM 51-00-00 PART 6 FIG 23 VERIFIED CRACK ENDS AT EXISTING FASTENER HOLE. FABRICATED DOUBLER FOR NR 7 SLAT INBD AREA IAW SRM 57-50-3 FIGOct 6, 2009 · N465FE · Boeing 727225 · Leading Edge DevicesSDR FDEA200910063494Vertical Beam · misinstalledAFT CARGO COMPT, BS 1183 PRESSURE BULKHEAD LBL 17.8 VERTICAL BEAM INBD FLANGE FASTENERS HAVE IMPROPER SPACING IN 4 AREAS. REPAIRED AFT CARGO COMPARTMENT BS 1183 PRESSURE BULKHEAD IAW EA NR 7-53-10-126851.Oct 6, 2009 · N465FE · Boeing 727225 · Fuselage Main, StructureSDR 07FDEA04774Accessory Unit · failedAFTER TAKEOFF, WITH GEAR RETRACTED, WHEN WE WENT FROM FLAPS 5 TO FLAPS 2 GOT THE TAKEOFF WARNING HORN, WOULD ONLY EXTINGUISH BY REDUCING POWER. ALSO GOT THE HORN WHEN WE WENT FROM FLAPS 25 TO FLAPS 30 AT LANDING. R & R MLG ACCESSORY UNIT IAW MM 32-09-121-4 Nov 13, 2007 · N465FE · Boeing 727225 · Landing Gear Retraction/Extension SystemSDR 07FDEA04138Wire · damagedAFT AIRSTAIR LIGHT ILLUMINATED AT ROTATION. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 30SEP07 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT, INOP. PLEASE WORK IN CONJUNCTION WITH TSI: 52-62 9704. REPAIRED WIRE AT SW S273 (UPLOCSep 20, 2007 · N465FE · Boeing 727225 · Door System WiringSDR 07FDEA02223Display · burnedPDIS 465 26-12 0009505 20JUN07 PIT OPEN R LOGPAGES: 01339908 APPROX 1 00 HOURS INTO FLIGHT, ALL CREWMEMBERS SMELLED A BURING SMELL AND SAW LIGHT SMOKE, SOURCE UNKNOW. PREFORMED PHASE ONES RED TAB PROCEDURE. DIVERTED INTO KPIT ENT BY: 001395 RPJun 20, 2007 · N465FE · Boeing 727200 · Central WarningSDR 07FDEA02041Seat Track · corrodedCABIN FLOOR SEAT TRACK HAS CORR, FS 460-620, RBL-24". REMOVED CORRODED SEAT TRACK AT RBL 24 , STA 480 TO 620 IAW B727 SRM 53-10-5. FAB NEW SECTION OF SEAT TRACK PO 1142187. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-Jun 1, 2007 · N465FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01985Stringer · corrodedFWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS- 720F-740. JUST O/B OF DUCT. REMOVED CORRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/NMay 26, 2007 · N465FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 07FDEA01984Stringer · corrodedFWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS-720F-740. JUST O/B OF DUCT. REMOVED CORRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/N#6May 26, 2007 · N465FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 07FDEA01980Skin · misrepairedEXTERNAL REPAIR ON FUSELAGE SKIN STA 1111-1127 AND STR 21R-23R DOES NOT COMPLY PER SRM. REMOVED OLD REPAIR IAW SRM 51-30-2. FABBED NEW DOUBLER IAW SRM 53-30-3 FIG 1 FROM MAT.2024T3 0.05, TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW DOUBLER IAW SRM 53-3May 25, 2007 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA01979Seat Track · corrodedCABIN FLOOR SEAT TRACK HAS CORROSION FS 640 LBL 1". REMOVED CORROSION IAW 727 SRM 51--10-2 FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL IAW SR 53-10-1. FABBED NEW SEAT TRACK IAW SRM 51-30-2 ,TREATED AND PRIMED IAW SRM 51-10-1. REMOVED AND INSTALLED SEAMay 25, 2007 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01978Stringer · corrodedFWD CARGO COMPT FS 720D-720E STR-26L HAS CORROSION. CUT OUT DAMAGE IAW SRM 53-30-3 FIG 5. FABBED REPAIR DOUBLERS AND FILLER IAW SRM 53-30-3 FIG 5. INSTALLED DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.May 25, 2007 · N465FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 07FDEA01841Web · corrodedAFT CARGO STA 970 S-28R WEB HAS CORROSION. REMOVED CORROSION ON WEB AT STA 970 STR 28R CORROSION FOUND OUT OF LIMITS IAW SRM 51-10-6, FABED NEW WEB ON MAE TR T7/679785. INSTALLED THE NEW WEB IAW SRM 51-30-2. INSTALLED STIFFENERS THAT WERE REMOVED PREVIOUSLYMay 17, 2007 · N465FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01840Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED UPPER SURFACE FROM FSTA 848 - 870, LBL 45 BLENDED SEAT TRACK AT 848 - FS870 LBL 45 FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-30-1 (FIG 1); ORDERED NEW SEAT TRACK PART NR BAC1520-841 BATCH NR 3370-1 AND LOCATED AND DRILLED May 17, 2007 · N465FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA01712Bracket · crackedNR 3 PYLON HOLE "P" BRACKET CRACKED FWD OUTBD SEEN INSIDE PYLON AS PER STEP4. 2 ON W/C 7-5410-7-3304. REMOVED AND REPLACED ANGLE( 69-16917-2) IAW SRM 51-30-2 AND 51-10-4. NDT CHECKED "P" HOLE FOR CRACK AND NO CRACK NOTED IAW NTM 51-00-11.May 7, 2007 · N465FE · Boeing 727225 · Nacelle/Pylon Miscellaneous StructureSDR 07FDEA01711Spar Cap · crackedRT WING UPPER SURFACE AT SPOILER PANEL NR 11 AREA SPAR CAP HAS CRACK AROUND 3RD HINGE FITTING. NDT NOTED NO CRACKED PER NTM 51-00-00 PT6 (AFTER STOP DRILL). STOP DRILLED 0.025" HOLE AT THE END OF CRACKED IAW SRM 57-30-4 FIG10 SHEET 1/3. TREATED AND PRIMED IMay 7, 2007 · N465FE · Boeing 727225 · Wing SparSDR 06FDEA04136Steering Sys · malfunctionedDURING TAKEOFF ROLL, A/C DRIFTED LEFT OF CENTERLINE WITH NO ABILITY TO CONTROL, TAKEOFF ABORTED. SUSPECTED ICY RUNWAY. DURING TAXI IN, NOTICED THAT THE RUDDER PEDALS WOULD NOT STEER A/C TO RIGHT, TILLER WAS REQ'D TO EFFECT RIGHT TURN. RIGHT RUDDER PEDAL DOENov 29, 2006 · N465FE · Boeing 727225 · Landing Gear Steering SystemSDR 05FDEA04388Switch · malfunctionedPASSING FL250 RECEIVED INTERMITTENT LE FLAPS AMBER INDICATOR ON FORWARD PANEL WITH INTERMITTENT NR1 SLAT INDICATOR ON S/O AUX PANEL. RAN RED TABS WITH NORMAL EXTENSION TO FLAPS 30. REPLACED NR 1 SLAT RETRACT SWITCH IAW 27-82-011-4, REPLACED NR1 SLAT ACTUADec 21, 2005 · N465FE · Boeing 727200 · Leading Edge Slat Control SystemSDR 05FDEA03246Seat Track · corrodedSEAT TRACK STA 600-620 AT LBL 45 IS CORRODED. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED SEAT TRACK REPAIR AT STA 590-690 ON LBL45 ALL IAW FX B727-200 SRM 53-10-5, 51-3-2 AND 51-10-2.Oct 5, 2005 · N465FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03245Seat Track · corrodedSEAT TRACK STA 480-620 LBL 24 FLANGE HAS CORROSION. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK AT STA 480-690 ON LBL 24 ALL IAW FX B727 SRM 53-10-5, 53-10-2, 51-30-2 AND 51-10-2.Oct 5, 2005 · N465FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03244Seat Track · corrodedSEAT TRACK AT LBL 45 STA 690-740 IS CORRODED. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK FROM STA 680-740 AT LBL45 ALL IAW FX B727-200 SRM 53-10-5,53-10-1 FIG 3, 51-30-2 AND 51-10-2.Oct 5, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03181Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA. 344 FROM BL 12 L TO BL 12 R. REMOVED CORROSION FROM FLOOORBEAM UPPER CAP IAW FED-EX SRM 53-10- 1. REMOVED, FABRICATED AND INSTALLED SPLICES AND FLOORBEAM IAW SRDM SR27-53-007, B727 SRM 51-10-2,51-30-2.Sep 30, 2005 · N465FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 05FDEA03178Seat Track · corrodedSEAT TRACK LBL 24 HAS 2 SPLICES AND CORROSION STA 380 - STA 480. REMOVED CORROSION, MATERIAL LOSS FOUND OUT OF LIMITS, ORIGINAL THICKNESS .085 MATERIAL REMOVED .029 RAMAINING .056, REMOVED SEAT TRACK. FABRICATED, DRILLED TO FIT, ALODINED, PRIMED AND INSTALLESep 30, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03146Floorbeam · corrodedCORRODED FLOORBEAM FS 620 FROM LBL 24 - LBL 45 THREE HEAVY AREAS. REMOVED, FABRICATED, ALODINED, PRIMED, HEAT TREATED, CAD PLATED AND INSTALLED FLOORBEAM REPAIR AT STA 620 FROM LBL24-45 ALL IAW FX DWG SR27-53-034E REPAIR NR 4 B727SRM 51-10-2,BAC5619H AND ASep 27, 2005 · N465FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 05FDEA03063Seat Track · corrodedSEAT TRACK INBOARD FLANGE HAS CORROSION BS 700 TO BS 740 LBL 24.Sep 22, 2005 · N465FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01759Transmitter · malfunctionedON TAKEOFF WITH STANDARD EPR SET NR3 N1,N2 AND FUEL FLOW WERE LOW. AC RELEASED FOR SERVICE IAW MEL/CDL: 77-01-01 01JUL05 14:55 ORF REMOVED PT2 SENSOR FROM ENG, BLEW AIR THROUGH LINE TO INSURE NO OBSTRUCTIONS PRESENT. RE-INSTALLED SAME. DISCONNECTED NR3 Jul 1, 2005 · N465FE · Boeing 727200 · Power Indicating SystemSDR 05FDEA00230Warning Light · illuminatedDURING MANUAL EXTENSION WHEN NOSE GEAR WAS UNLOCKED, BOTH MAINS SHOWED UNSAFE. JACKED ACFT, PERFORMED NOSE GEAR MANUAL EXTENSION, SYSTEM TEST SEVERAL TIMES WITH FLAPS AT DIFFERENT SETTINGS AND PRESSURE ON AND OFF. SYSTEM FUNCTIONAL CHECKS GOOD IAW FED EX M/MFeb 2, 2005 · N465FE · Boeing 727200 · Landing Gear Position and Warning
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