N273FE, cancelled Aug 27, 2013

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 = 'N273FE' AND deregistration_id = 'N273FE-2013-08-27'
  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 FDEA201009283775Engine · failedLOUD BANG/ ACFT SHUDDER DURING TAKEOFF, ACFT TAKEOFF REJECTED AT 115 KNOTS. GROUND PERSONNEL REPORTED HEARING 3 DISTINCT LOUD BANGS, NO APPARENT ENGINE MALFUNCTION NOTED PRIOR TO REJECT (ON GAUGE) WITH ALL INDICATIONS NORMAL AT IDLE. INSPECT ALL THE ACFT AISep 28, 2010 · N273FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR FDEA201002130419Inlet · obstructedLT AND RT PACK "TRIP OFF" LIGHTS W/ "DUCT OVER" LIGHT. ON POST FLIGHT, PACK COOLING DOOR FILLED WITH SNOW. INSPECTED PACK INTAKES AND FOUND SNOW PACKED INSIDE. MELTED SNOW FROM PACK INLET AREA. OPERATED PACKS IAW MM 21-61-000-5 AND 21-55-000-5. OPS CHECK Feb 13, 2010 · N273FE · Boeing 727233 · Cabin Cooling SystemSDR FDEA200909233364Motor · leakingLOST SYS A HYD FLUID DURING CLIMBOUT DID QRH CHECKLIST. SECURED SYS A HYD PUMPS AND CLOSED FLUID SHUTOFF SWITCHES IAW QRH. REMOVED AND REPLACED BOTH FLAP MOTORS IAW 27-51-062-4, REMOVED AND REPLACED ENG NR 1 AND 2 CASE DRAIN FILTERS IAW 29-11-041-2, REMOVED SSep 23, 2009 · N273FE · Boeing 727233 · Hydraulic System, MainSDR 08FDEA03042Channel · corrodedLOWER FUSE WING BODY FILLET FRG SUPPORT FRAME U CHANNEL IS CORRODED BS 773, LBL 9 - RBL 9, WL 140. REMOVED U CHANNEL REF SRM 51-30-2. FABRICATED "U" CHANNEL ON SHOP SNRM NR N00692, DRILLED UP, TREATED, PRIMED AND PAINTED "U" CHANNEL REF DWR 65-58504, SRM 51Jul 24, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02994Intercostal · corrodedDELTA BEAM AT STA 740 HAS CORROSION AROUND AND UNDER HEADS OF SEVERAL FASTENERS. CAN BE SEEN THRU ACCESS HOLE BELOW BEAM. REMOVED CORROSION. ORIGINAL "T" .107 LOSS AT LOWEST POINT IS .028 REMAINING "T" IS .079. OUT OF LIMITS REF SRM 53-10-1 FIG 101 DETAIJul 21, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02985Bracket · crackedNR 1 ENG UPPER COWL, BRACKET CRACKED AT FWD O/B LOWER CORNER REMOVED AND REPLACED CRACKED SEGMENT, PAINTED AFFECTED AREA OF COWLING. REF SRM 51-30-2 PG 2, MM 51-20-151-7 PG1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 19, 2008 · N273FE · Boeing 727233 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA02984Fairing · crackedRT BODY FAIRING PANEL NR 3349 CRACKED AT EDGE. REMOVED DAMAGED EDGE PLATE. VERIFIED MATERIAL FOR NEW EDGE PLATE, FABRICATED NEW EDGE PLATE, TREATED AND PRIMED AND INSTALLED. REF DWR 65-58505 AND SRM 51-10- 2 PG1, 51-30-2 PG1. THIS IS CLASSIFIED AS A MINORJul 19, 2008 · N273FE · Boeing 727233 · Aerodynamic FairingsSDR 08FDEA02983Retainer · corrodedLEFT MLG W/W LOWER FWD WING PANEL HAS CORROSION ON SEAL RETAINER STRIP NEAR LOWER MLG SUPPORT BEAM, WSS 217. REMOVED AND REPLACED LEFT MLG W/W LOWER FWD WING PANEL SEAL RETAINER AT WSS 217 REF SRM 51-30-2 PG 2 AND DWR 65-21656. THIS IS CLASSIFIED AS A MINOR Jul 19, 2008 · N273FE · Boeing 727233 · Wing Miscellaneous StructureSDR 08FDEA02958Bulkhead · corrodedCORROSION AT BS 1166 BULKHEAD RT SIDE "T" ANGLE (AT BOTTOM NUTPLATE AFT SIDE OF BULKHEAD). REPLACED T-CHORD AT AFT PIT BULKHEAD BS 1166 RBL 25 INCHES. REMOVED CORROSION AND FOUND NOT WITHIN ALLOWABLE LIMITS ORIG MATERIAL THICKNESS IS .063, MATERIAL LOSS IS .Jul 17, 2008 · N273FE · Boeing 727233 · Fuselage Main, BulkheadSDR 08FDEA02954Floor Support · corrodedUNDER FWD LAV STA 328 TO 344 FLOOR SUPPORT RBL 52 HAS CORROSION AROUND NUTPLATES REMOVED AND REPLACED SUPPORT FROM STA 326-344 RBL REF SRM 51-30-2 PG 2, FLOOR SUPPORT AT RBL 52 STA 328-344. FOUND TO BE WITHIN LIMITS OF SRM 53-10-06, TREATED AND PRIMED REF SRMJul 17, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02949Web · crackedRIGHT WING O.B. L.E. NR 5 SLAT BN 279, CRACKED LWR. AFT INTERNAL WEB ANGLE AT INBD. SIDE OF ACTUATOR RAM ATACH STRUCTURE REMOVED ACCESS PANEL, INSPECTED FOR CRACKS, VERIFIED MATERIAL, FABRICATED, LOCATED AND DRILLED REPAIR PART. INSTALLED REPAIR, INSTALLED ACJul 17, 2008 · N273FE · Boeing 727200 · Leading Edge DevicesSDR 08FDEA02926Floor Support · corrodedFLOORBOARD, FWD LAV SUPPORT NUT PLATES RUSTED STA 305 - RBL 44. REMOVED FLOOR SUPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIG. MATERIAL THICKNESS .040 INCH. REMAINING .031 INCH REMOVED .009'. FABRICATED NEW ANGLE, PENATRANT INSP FOR CRACJul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02945Panel · delaminatedUPPER TAIL PANEL NR 9607, INNER FOIL DISBONDED REPAIRED TEDLAR COVERING ON INNER SURFACE REF SRM 51-40-9 STEP 11 PG 18. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 16, 2008 · N273FE · Boeing 727233 · Horizontal Stabilizer, Plate/SkinSDR 08FDEA02939Panel · crackedPANEL 3617 BOTTOM AFT END CRACKED REPAIRED PANEL 3617 REF SRM 51-40-9 STEPS 3D, 4E, 4F, PGS 3-7 AND AMM 51-20-051 PG1, AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 16, 2008 · N273FE · Boeing 727233 · Wing, Plate/SkinSDR 08FDEA02938Panel · delaminatedNR 3 SLAT UNDERWING PANEL NR 6224 HAS AREA OF DELAMINATION REPAIRED PANEL 6224 REF SRM 51-40-9 STEPS 3D, 4E, 4F PG3-7 AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 16, 2008 · N273FE · Boeing 727233 · Leading Edge DevicesSDR 08FDEA02927Door · gougedMAIN CARGO DOOR, AFT EDGE LOWER CORNER GOUGED LOWER AFT CORNER GOUGED BEYOND LIMIT. REMOVED DOUBLER FABRICATED NEW DOUBLER, TREATED AND PRIMED. INSTALLED NEW DOUBLER REF 727 P-FSRM 52-30-2 PG 1/2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 16, 2008 · N273FE · Boeing 727233 · Cargo/Baggage DoorsSDR 08FDEA02925Frame · corrodedRT AFT EMERGENCY EXIT HATCH LOWER FRAME OUTER SURFACE HAS CORROSION. REMOVED CORROSION REF SRM 52-00-2 NDT THICKNESS ORIGINAL "T" .063, .005 LOSS, .058, DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED PRIMED AND PAINTED REWORKED AREAS REF Jul 16, 2008 · N273FE · Boeing 727233 · Emergency ExitsSDR 08FDEA02924Frame · corrodedRIGHT FWD EMERGENCY HATCH FRAME LOWER OUTER SURFACE CORRODED BETWEEN SEAL RETAINER AND SKIN REMOVED CORROSION REF SRM 52-00-2. NDT THICKNESS ORIG "T" .063 LOSS .005 .058. REMAINING DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED, PRIMED AJul 16, 2008 · N273FE · Boeing 727233 · Emergency ExitsSDR 08FDEA02922Skin · crackedLEFT WING INBD AFT FLAP, 3RD ATTACH FITTING OUTBD SKIN CRACKED FABRICATED REPAIR PARTS AT LEFT WING T/E AFT FLAP, THIRD ATTACH FITTING O/B SKIN, REF 27-50-4 FIG 11. TREATED, PRIMED AND INSTALLED, REF SRM 51-20-2 PG 1-7, 57-50-04 FIG 11, 51-30-2 PG 2-4. PAIJul 16, 2008 · N273FE · Boeing 727233 · Trailing Edge FlapsSDR 08FDEA02921Floor Support · corrodedFLOORBOARD SUPPORT NUTPLATES RUSTED STA 305-312 RBL 55 FWD LAV. REMOVED FLOOR SUPPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORIG MATERIAL THICKNESS .040, REMAINING .033, REMOVED .007. INSTALLED NEW ANGLE REF SRM 51-30-2 PG 2, SRM 53-10-1 PG 1Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02917Skin · corrodedC1 PIT BILGE AREA-STR 28R STA 680 LEVELING COMPOUND BULGING WITH CORROSION ON SKIN. REMOVED DAMAGED COMPOUND. FOUND CORROSION AT SKIN AND NDT FOR LIMITS ORIGINAL "T" .070 LOSS AT LOWEST POINT IS .034, REMAINING T IS .036 IS OUT OF LIMITS REF SRM 53-30-3. REJul 16, 2008 · N273FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA02916Floor Panel · corrodedMAIN DECK LAV FLOOR WEB PANEL, UPPER LWR SURFACES ARE CORRODED BS 304 - 340, RBL 40 - 60, WL 208. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .042 INCH, REMAINING .035', REMOVED .007. FOUND TO BE OUT OF LIMITS REF DRM 53-10-1 PG 2, TOOL ID AAR 9800 CAL DJul 16, 2008 · N273FE · Boeing 727233 · Fuselage Floor PanelSDR 08FDEA02915Floor Support · corrodedFWD LAV FLOOR SUPPORT STA 305-312 RBL 42 NUTPLATES RUSTED AND FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM, ORIGINAL THICKNESS .070, REMAINING .066. REMOVED .004, FOUND TO BE WITHIN LIMITS, REMOVED CORROSION FROM FLOOR SUPPORT, ORIG THICKNESS.070, Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02913Channel · crackedE/E DOOR CUT-OUT FWD ANGLE CRACKED BY LATCH REPLACED CUT OUT FWD ANGLE AND RIGGED E/E DOOR REF BOEING DWR 65-16351, SRM 51-30-01 PG 1-10, SRM 51-30-5 PG 3, SRM 51-30-2 PG 2/3, AMM 51-20-151 PG 1-6, AMM 20-60-001 PG10, MM 52-40-011 PG 1. THIS IS CLASSIFIED AS Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02841Angle · corrodedBS 740 BULKHEAD LOWER FWD SURFACE, ANGLE LBL 4.5 TO RBL 4.5, WL 146.5 HAS CORROSION ON AFT SURFACE FABRICATED NEW ANGLE REF SRM 51-10-2 PG 2, DWR 65-23555. TREATED AND PRIMED REF 51-10-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 12, 2008 · N273FE · Boeing 727233 · Fuselage Main, BulkheadSDR 08FDEA02834Fitting · corrodedBS 740 BULKHEAD LOWER SURFACE, "T" ANGLE AT RBL 5" WL 146.5 CONNECTION TO DELTA BEAM "T" FLANGE IS CORRODED NEW T ANGLE FABRICATED ON SHOP NON-ROUTINE N00670. REMOVAL AND INSTALLATION ACCOMPLISHED ON N00167. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 12, 2008 · N273FE · Boeing 727233 · Fuselage Main, BulkheadSDR 08FDEA02796Structure · crackedNUMBER 3 CARGO DOOR LOWER FWD "T" CHORD CRACKED AT FASTENERS REPAIRED LOWER FWD "T" CHORD. REMOVED LWR INNER DOOR SKIN REF SRM 51-30-2. FABRICATED REPAIR ANGLES AND FILLER REF SRM 51-40-04 PG 14-16 FIG 3. TREATED AND PRIMED REPAIR PARTS REF SOPM 20-44-04 PGJul 9, 2008 · N273FE · Boeing 727233 · Cargo/Baggage DoorsSDR 08FDEA02780Support Bracket · corrodedCORROSION AROUND BOLT HOLE AT STA 340 FITTING SUPPORT BRACKET JUST BEHIND NOSE WHEEL WELL LT SIDE. REMOVED FITTING SUPPORT AT STA 340 AFT OF NOSE WHEEL WELL LT SIDE. TREATED AND PRIMED NEW SUPPORT FITTING REF SRM 51-30-2 PG 1-20 AND MM 51-20-7. THIS IS CLASJul 9, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA02778Retainer · corrodedRT WING REAR SPAR LWR CHORD, APPROX 12" IB OF FWD MLG TRUNNION, SEAL RETAINER CORRODED AT OB END. REMOVED FAIRING AND SEAL RETAINER REF SRM PG 2 LOCATED AND DRILLED NEW SEAL RETAINER REF SRM 51-30-5 PG 1, INSTALLED SEAL RETAINER AND FAIRING REF SRM 51-30-2Jul 9, 2008 · N273FE · Boeing 727233 · Wing Miscellaneous StructureSDR 08FDEA02777Frame · corrodedLWR AFT CARGO PIT, CORROSION ON UPPER FLANGE OF FRAME AT STA 1090 STR 27L REMOVED CORROSION, ORIGINAL "T" .063, REMOVED .017, REMAINING .046 OUT OF LIMITS. FABRICATED REPAIR DOUBLER FROM 7075-0 .063, HEAT TREAT T6, APPLIED ALODINE, PRIMER AND INSTALLED REPAIJul 9, 2008 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA02739Slat · crackedLT WING NR 4 SLAT FENCE UPPER AFT END COMPOSITE IS CRACKED AND DELAMED. REPAIRED NR 4 SLAT FENCE REF SRM 51-40-9 STEP 7 PG 9 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 8, 2008 · N273FE · Boeing 727233 · Leading Edge DevicesSDR 07FDEA01818Line · failedAFTER TOUCHDOWN AMD SPOILER DEPLOYMENT, EXPERIENCED LOSS OF "A" HYDRAULIC SYSTEM QUANTITY AND PRESSURE. FOUND BLOWN FLEX LINE ON LT ELEVATOR PCU. PART IS IN STOCK AT SAV. REMOVED AND REPLACED I/B FLEX LINE PER MM27-30-081-4. SERVICED "A" HYD SYS TO FULL PEMay 15, 2007 · N273FE · Boeing 727233 · Hydraulic System, MainSDR 06FDEA1317Pressure Switch · malfunctionedAT FL350, AND FUEL TEMPERATURE 5, NR 2 FUEL ICING LIGHT ILLUMINATED. PERFORMED RELEVANT EMERG CK-LIST. DECLARED EMERGENCY. RELEASED FOR SERVICE PER MEL/CDL: 73-04 CATEGORY: C "MEL 73-04. TWO FUEL FILTER DIFFERENTIAL PRESSURE WARNING SYSTEM INOP. REMOVED AApr 6, 2006 · N273FE · Boeing 727233 · Fuel Flow SensorSDR 06FDEA0499Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT FS 500 STR.30 WAS ACCOMPLISHED IAW SRM 53-30- 3, FIG. 24 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION OF THE REPAIR, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE, THICKNESS, GENERAL WORKMANSHFeb 2, 2006 · N273FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0472Repair · unknownFOUND PREVIOUSLY INSTALLED REPAIR AT AFT INBD CORNER OF PNEUMATIC GROUND CONNECTION CUTOUT WAS DETERMINED TO BE IAW SR 27-53-024, BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND Feb 1, 2006 · N273FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01785Switch · malfunctionedON FLAP RETRACTION FROM 5 DEG TO 2 DEG, LED NR 5 (RT SIDE) DID NOT FULLY RETRACT. AMBER LIGHT ILLUMINATED ON LED POSITION INDICATOR AFT BULKHEAD. COMPLIED WITH RED TABS, DID NOT CORRECT PROBLEM. REMOVED AND REPLACED NR 5 L/E FLAP POSITION SWITCH IAW MM 27-8Oct 21, 2003 · N273FE · Boeing 727200 · Leading Edge Slat Control SystemSDR 03FDEA00885Skin · dentedFUSELAGE SKIN HAS A DENT, STRINGER 6L, BS 720C. REPAIR DENTED SKIN PER SRM 53-30-3 FIG 3.Jun 16, 2003 · N273FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00886Skin · corrodedCORROSION (C53-113-01, 2) BULGING SKIN ON STR 28L, BS 1055.Jun 16, 2003 · N273FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00838Warning Light · illuminatedDURING FLAP RETRACTION FROM FLAPS 2 TO FLAPS UP. LED AMBER LIGHT REMAINED ILLUMINATED. POSITION TEST SELECTOR INDICATED NR 2 LED WAS STILL EXTENDED, NR 2 SLAT.Nov 14, 2002 · N273FE · Boeing 727200 · Leading Edge Slat Position Indicating SystemSDR 01FDEA00018Skin · crackedCRACK IN SKIN, VERTICAL STAB, LEFT SIDE, STR 10, BOTTOM OF STAB. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 55-30-3 AND FEDEX EA 7-5510-56226.Jan 11, 2001 · N273FE · Boeing 727233 · Elevator, Plate/SkinSDR 01FDEA00014Frame · dentedFRAME IS DENTED AT BS 520, STRINGER 22 RT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3.Jan 9, 2001 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00011Doubler · gougedMAIN CARGO DOOR AFT FRAME BS 620 IS GOUGED AT PREVIOUS REPAIR. INGD RADIUS APPROX 21 INCHES UP FROM THE BOTTOM EDGE. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-40-3. PREVIOUS REPAIR. INSTALL REPAIR DOUBLER PER IAW FEDEX SRM 51-30-2.Jan 8, 2001 · N273FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 01FDEA00003Stringer · damagedNR 319 TEN OPEN FASTENER HOLES ON SIDE OF STRINGER 24 LT AT BS 480. ** S/D ** R&R & FAB PER FEDEX SRM 53-10-3, 53-10-3.Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00004Stringer · crackedCRACK AT STR 15 LT SIDE BS 720C-4 AFT OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00005Stringer · crackedNR 419 CRACK AT STR 15 LT SIDE BS 720D+4 FWD OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00006Stringer · crackedNR 420 CRACK AT STR 15 RT SIDE BS 720B+4 FWD OF EXT LIGHT. ** S/D ** COMINGJan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00002Keelbeam · corrodedCORROSION ON LT KEELBEAM AT BS 960 O/B FLANGE AROUND FASTENERS. ** S/D ** COMINGJan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, KeelSDR 00FDEA00753Switch · out of adjRT MG DOOR REMAIN ILLUM AFT GEAR RETRACTION GOES OUT IN UP POSITION. *S/D* ADJUSTED RT GEAR DOOR SWITCH PER 2 B (2) OF MM 32-62-11-4.Nov 1, 2000 · N273FE · Boeing 727233 · Landing Gear Position and WarningSDR 98FDEA00512Bellframe · damagedNR 0546 - LOWER AFT CARGO COMP FS 1010 BELLFRAME BETWEEN STRINGERS 25L AND 26L CREASED. REMOVED DAMAGED AREA. FABRICATED DOUBLERS, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-4.Aug 5, 1998 · N273FE · Boeing 727233 · Fuselage Main, FrameSDR 96FDEA00133Floorbeam · corrosionCORROSION ON FLOORBEAM BS 460 RBL 10 AND 15 WL 208. REPAIRED FLOORBEAM AT BS 460 RBL 10 TO 15 WL 208. ALL WORK DONE IAW FEDEX EA 7-5310-26943.Jan 26, 1996 · N273FE · Boeing 727233 · Fuselage Main, Floor Beam
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