Boeing 727-2S2F

Service difficulty reports · 842

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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 = '7272S2F'
  ORDER BY difficulty_date DESC"

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SDR 08FDEA04661Floor Support · corrodedMAIN DECK FLOOR SUPPORT INTERCOSTAL IS CORRODED BS 304-312, LBL 30, WL 230 REMOVED CORROSION ON INTERCOSTAL AT BS 304-312 ORIGINAL THICKNESS .062, MATERIAL LOSS .012 REMAINING MATERIAL .050 OUT OF LIMITS. REMOVED INTERCOSTAL AND FABRICATED NEW INTERCOSTAL INSNov 1, 2008 · N216FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA03520Fitting · corrodedGENERATED BY EO 7-5510-7-5000, HORIZONTAL STAB RT HINGE FITTING O/B BUSHING BORE HAS CORROSION OVERSIZED LUG BORE TO 2.2244 INCH CORROSION REMOVED. HFEC INSPECTED BORE NO DEFECTS NOTED. FABRICATED OVERSIZE BUSHING, CAD PLATED BUSHING. INSTALLED OVERSIZE BUSAug 20, 2008 · N211FE · Boeing 7272S2F · Horizontal Stabilizer, Attach FittingsSDR 08FDEA03498Support Angle · corrodedRT WHEEL WELL, LOWER FUSELAGE FAIRING SUPPORT FRAME HAS CORROSION, RBL 21, STA 950 FABRICATED TEE ANGLE FROM RT WHEEL WELL FUSELAGE FAIRING SUPPORT STA 950 REFB DWR 65-25550 AND CUSTOMER REQUEST, HEAT TREATED TRACKING NUMBER 2008-08-057. TREATED AND PRIMED, RAug 19, 2008 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA03456Bracket · crackedAIRSTAIR COMPARTMENT LT BRACKET FOR FIRE LOOP SUPPORT IS CRACKED AT BULKHEAD STA 1183 NEAR FLOOR LEVEL. REMOVED OLD BRACKET REF SRM 51-30-02 P 1-7, IDENTIFIED MATERIALS REF DWR 65-27195 FRAME 1 SHEET 3 REV E ALSO A-TAG NR A03329. FABRICATED NEW BRACKET REF DAug 16, 2008 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA03455Beam · corrodedLT MLG W/W UPPER BOX BEAM LOWER WEBS AFT OF STA 910 AND 930 HAVE CORROSION REMOVED FASTENERS FOR ACCESS. REMOVED CORROSION, ORIGINAL .080 REMAINING .070. REMOVED .010 OUT OF LIMITS, FABRICATED REPAIR DOUBLER 7075-O-100 HEAT TREAT T6. APPLIED ALODINE AND PRIAug 16, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, StructureSDR 08FDEA03451Fairing · crackedRT WING NR 6 FLAP TRANSMISSION FAIRING IS CRACKED AT CENTER ATTACH HOLE REMOVED FAIRING REF 51-30-2, PG 1-7 STOP DRILLED CRACKS REF 727 SRM 51-10-1 PG 13. NDT VERIFIED CRACK CONTAINMENT. NDT MANUAL PART 6, 51-00-00 FIG 23. ORIGINAL AND REPAIR MATERIAL IDENTAug 16, 2008 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA03449Fairing · crackedNR 5 FLAP TRACK MIDDLE FAIRING, AFT SKIN BENT/CRACKED. REMOVED DAMAGED SKIN, REF 51-30-2, PG 1-7. ORIGINAL SKIN AND REPLACEMENT BOTH IDENTIFIED AS 7075-T6, .040 REF 65-21795, REV E, PG 35 AND DWG 65-21795, AND A-TAG NR A27927. FABRICATED NEW SKIN, REF SRM 5Aug 16, 2008 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA03448Attach Angle · crackedRT WING, LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR I/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 16, 2008 · N211FE · Boeing 7272S2F · Wing, Attach FittingsSDR 08FDEA03447Attach Angle · crackedRT WING LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 16, 2008 · N211FE · Boeing 7272S2F · Wing, Attach FittingsSDR 08FDEA03446Bracket · crackedFWD NOSE COMPARTMENT WEATHER RADAR MOUNT BRACKET CRACKED REMOVED WEATHER RADAR R/T. REPLACED MOUNT BRACKET, INSTALLED WEATHER RADAR R/T AND PERFORMED GOOD OPS CHECK REF SRM 51-30-02, AMM 34-41-041-4 AND AMM 34-41-000-5. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 16, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, Attach FittingsSDR 08FDEA03407Angle · crackedLT WING ROOT TE UPPER PNL IB OF NR 7 SPOILER HAS FRETTED/CRACKED IB SUPPORT ANGLE BS 950A, WBL 70. REPLACED SUPPORT ANGLES REF SRM 51-30-02 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 13, 2008 · N211FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 08FDEA03406Angle · crackedLEFT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 4 SLAT WELL. REMOVED INTERCOSTAL AND DAMAGED SUPPORT ANGLE, FABRICATED NEW SUPPORT ANGLE, HEAT TREAT "T-3". TREAT AND PRIMED SUPPORT ANGLE, INSTALLAug 13, 2008 · N211FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 08FDEA03403Duct · crackedRT EXT FUSE NR 3 ENG FAN AIR EXH PORT ASSY IS FRETTED/CRACKED. REMOVED AND REPLACED FAN AIR EXH POT ASSY REF SRM 51-30-2 PG 1-32, REF MM 51-20-151-7 PG 1-5, REF MM 36-00-001-2 PG 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 13, 2008 · N211FE · Boeing 7272S2F · Pneumatic Distribution SystemSDR 08FDEA03402Frame · corrodedLWR EXT FUSE BODY FRAME LWR CHORD IS CORRODED BS 351, LBL 17, WL 148-150. REMOVED CORROSION AT LWR EXT FUSE BODY FRAME LWR CHORD STA 351 LBL 17 - RBL 17, REF SRM 51-10-6 PG 1-5. MATERIAL LOSS 50 PERCENT, FOUND OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED ANAug 13, 2008 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA03401Support Angle · crackedRIGHT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 5 SLAT WELL. REMOVED INTERCOSTAL AND SUPPORT ANGLE AT SLAT STA 260. FABRICATED NEW SUPPORT ANGLE. VERIFIED MATERIAL 2024 T-3, FAB'D WITH 2024-0, Aug 13, 2008 · N211FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 08FDEA03400Floorbeam · crackedMAIN DECK FLOORBEAM INTERCOSTAL MID CHORD EXISTING REPAIR DOUBLER IS CRACKED BS 302, WL 207 FABRICATED NEW REPAIR ANGLE REF SRM 51-40-3 PG 1. TREATED AND PRIMED REF SRM 51-10-2 PG 1-9. INSTALLED ANGLE REF SRM 51-30-2 PGS 1-7. THIS IS CLASSIFIED AS A MINOR RAug 13, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 08FDEA03391Bracket · corrodedCORROSION ON RT A/C BAY FWD COMPARTMENT LIGHT LENS RETAINER AND LIGHT MOUNT BRACKET. REPLACED FWD COMPARTMENT LIGHT, LENS RETAINER AND LIGHT MOUNT BRACKET. REFERENCE SWPM 20-84-10, PG 3-5; SRM 51-30-02 PG 2-3; BOEING DRW NR 66-14827-1/1. OPERATIONAL TEST OFAug 12, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, Attach FittingsSDR 08FDEA03390Duct · crackedBLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON CRACKED AT AFT EDGE OF OPENING. REMOVED AND REPLACED BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON. REF IPC 36-10-00-10 FIG 10, SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 12, 2008 · N211FE · Boeing 7272S2F · Engine Bleed Air SystemSDR 08FDEA03389Bracket · crackedL-1 GRAB ASSIST HANDLE MOUNT BRACKET CRACKED ON DOOR REPLACED FWD ENTRY DOOR ASSIST BRACKET REF: SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 12, 2008 · N211FE · Boeing 7272S2F · Passenger/Crew DoorsSDR 08FDEA03388Fairing · crackedPANEL RACK, WING BODY FAIRING 3517 AFT CORNER EXISTING COMPOSITE REPAIR IS CRACKED. REPAIRED PANEL 3517 REF SRM 51-40-9 STEP 7B(1)-7B(12) AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIRAug 12, 2008 · N211FE · Boeing 7272S2F · Aerodynamic FairingsSDR 08FDEA03354Fairing · crackedLEFT WING INBD T/E LWR SURFACE, NR 3 FLAP TRACK FAIRING INBD ATTACH L- ANGLE CRACKED BETWEEN 2 FASTENERS, 12 INCHES FWD OF T/E PANELS AFT EDGE. REMOVED DAMAGED PORTION OF NR 3 FLAP TRACK FWD FAIRING INBD ATTACH L- ANGLE. FABRICATED FILLER AND DOUBLER, AND Aug 9, 2008 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA03321Intercostal · crackedMAIN DECK FLOORBEAM INTERCOSTAL UPPER CHORD IS BUCKLED/CRACKED BS 304-312, LBL 22. FABRICATED REPAIR ANGLE REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-9. INSTALLED REPAIR REF SRM 51-30-2 PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 8, 2008 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA03302Fairing · crackedLEFT WING INBD TE NR 3 FLAP TRANSMISSION JACKSCREW FAIRING ON O/B END OF MID FLAP IS CRACKED OUT OF FWD UPPER HOLE REMOVED FAIRING. NDT VERIFIED CRACK LOCATION. REMOVED DAMAGE AND INSTALLED REPAIR. REINSTALLED FAIRING TO MID FLAP REF SRM 51-30-2 PG 13/ NDT Aug 7, 2008 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA03301Fairing · crackedLEFT WING OB TE NR 2 FLAP TRANSMISSION JACKSCREW FAIRING ON INBD END OF MID FLAP HAS CRACK IN SIDE WEB 19 INCH AFT OF FWD END REMOVED CRACKED WEB. FABRICATED NEW WEB, P/N 65-28131-1. TREATED, PRIMED, AND PAINTED WEB. INSTALLED WEB REF SRM 51-30-2 PG 2-4/SRMAug 7, 2008 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA02553Control Unit · inoperativeIMMEDIATELY AFTER ROTATION, FIRE BELL ACTIVATED AND FIRE WARN LIGHTS ILLUMINATED. COULD NOT CANCEL BELL. FINALLY PULLED "FIRE BELL" CIRCUIT BREAKER. RAN FIRE TEST ON ENGINES AND MAIN CARGO COMPARTMENT. TESTED OK. REMOVED AND REPLACED ENGINE FIRE PROTECTIOJun 28, 2008 · N215FE · Boeing 7272S2F · Fire DetectionSDR 08FDEA01765Stringer · crackedSTRINGER 8R CRACKED AT RIB NR 8 STRINGER 8R, FIN STA 157.200 CRACK TERMINATES IN FASTENER HOLD AND HFEC INSPECTED AREA AND VERIFIED IAW NDTM 51.00.00 PART 6. FABRICATED REPAIR ANGLE IAW SRM 55.30.5 FIGURE 7. TREATED AND PRIMED AREA IAW SRM 51.10.2. INSTALLEMay 5, 2008 · N203FE · Boeing 7272S2F · Vertical Stabilizer, Spar/RibSDR 08FDEA01764Stringer · crackedSTRINGER 8L CRACKED AT RIB NR 8 STRINGER 8L, FIN STA 157.200 CRACK TERMINATES IN FASTENER HOLE AND HFEC INSPECTED AREA AND VERIFIED IAW NDTM 51.00.00 PART 6. FABRICATED REPAIR ANGLE IAW SRM 55.30.5 FIGURE 1. TREATED AND PRIMED PARTS IAW SRM 51.10.2. INSTALLMay 5, 2008 · N203FE · Boeing 7272S2F · Vertical Stabilizer, Spar/RibSDR 08FDEA01763Stringer · corrodedSTR 26 R HAS EXFOLIATION CORROSION BETWEEN STA 1010 AND 1030 CUT-OUT DAMAGED STRINGER SECTION (DIMENSION 12" LONG) AND FABRICATED HAT SECTION AND 1 SPLICER IAW SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED PARTS IAW SRM 51-10-2 AND INSTALLED RMay 5, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR 08FDEA01762Support · damagedLT IB MID-FLAP LOWER T/E CHORD WBL 104 ON PUSH-ROD CUT OUT IS CRACKED ON BOTH CORNERS CUT OUT DAMAGE AREA DIM CUT-OUT 47 1/4 INCH LONG IAW SRM 51-40-3 FIG 1. FAB NEW ANGLE "CHORD" 1 SPLICER IAW SRM 57-50-2 FIG 8 AND 51.40.3 FIG 1. TREATED AND PRIMED IAW SRMMay 5, 2008 · N203FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA01761Support Angle · crackedRT WING INBD MID-FLAP AFT LOWER SUPPORT ANGLE IS CRACKED 2 PLACES AT WBL 100. REMOVED I/B MID FLAP LOWER PANEL FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE SECTION DIM CUT OUT (61 INCHES BY 2 INCHES) IAW SRM 51-10-1, AND 51-40-4 FIG 3. FAB REPAIR ANGLE IAW SMay 5, 2008 · N203FE · Boeing 7272S2F · Trailing Edge FlapsSDR 08FDEA01703Skin · crackedCRACK IN LWR FUSELAGE AT STA 1055, 5.5 INCHES RIGHT OF CENTERLINE STR 29R. CUT-OUT DAMAGED AREA & FABRICATED REPAIR FILLER & REPAIR DOUBLER IAW SRM 53-30-3 FGIURE 3 & 53-30-2 FIGURE 2, TREATED & PRIMED PARTS IAW SRM 51-10-2 & INSTALLED REPAIR PARTS IAW SRM 53Apr 30, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA01643Control Box · failedFL 340 SCHEDULE CABIN 5200 FEET CABIN UNCONTROLLED CLIMB TO 126500 FEET. REMOVED AND REPLACED TEMP CNTL BOX IAW MM 21-55-091-5, CONTROL BOX AND THE 35 DEGREE CONTROL VALVE OPS CHECK NORMAL. REPLACED LEFT FLOW CONTROL MODULATING AND SHUTOFF VALVE REF M/M 36-Apr 28, 2008 · N215FE · Boeing 7272S2F · Cabin Temperature Control SystemSDR 08FDEA01644Web · crackedLT AIRSTAIR LWR TORQUEBOX OUTER WEB CRACKED AT LIGHTING HOLE BS 1329. TRIMMED OUT DAMAGED AREA IAW SRM 51-10-1, 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PART IAW SApr 28, 2008 · N203FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA01602Stringer · corrodedLWR FUSELAGE AFT PIT CORROSION ON 29L OUTBRD SIDE AND STA 1010 CLEANED AND EVALUATED AREA, NO CORROSION FOUND IAW B727 SRM 51-10-01 AND SOPM 20-30-03.Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR 08FDEA01608Stringer · corrodedLWR FUSELAGE STR 29 R AT STA 990 CORROSION ON SPARE TIES, CLIPS, AND TOP OF STRINGER. REMOVED CORROSION FROM SHEAR TIE IAW SRM 51-10-6, ORIG. MAT. 0.063, MAT. LOSS 0.004, REMAINING MAT. 0.059 AND FOUND WITHIN LIMITS IAW SRM 53-10-2, 53-10-1, CLEANED AREA CLApr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR 08FDEA01606Intercostal · corrodedLWR FUSELAGE AFT PIT CORROSION ON INTERCOSTAL AT STA 885 FROM 28L TO 29L. REMOVED CORROSION AND EVALUATED AREA ORIGINAL MAT 0.032, MAT. REMAINING 0.029, MAT LOSS 0.003". TREATED AND PRIMED IAW SRM 51-10-06, 51-10-01 FIG 1, 51-10-02 AND SOPM 20-30-03.Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA01605Stringer · corrodedLOWER FUSELAGE AFT PIT CORROSION ON 29R STRINGER FROM STA 885-890. REMOVED CORROSION AT AFT PIT ON STIFFENER , ORIG MAT 0.063, MAT LOSS 0.003, MAT REMAINING 0.060", TREATED AND PRIMED IAW SRM 51-10-01, 53-10-02, 53-10-01.Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR 08FDEA01599Stringer · corrodedCORROSION ON OUTBRD SIDE OF STRINGER 26L AT STA 1133 (AFT PIT). CLEANED AND EVALUATED AREA, NO CORROSION FOUND IAW SOPM 20-30-03, SRM 51-10-06 PAR. 3Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR 08FDEA01598Stringer · corrodedAFT PIT CORROSION ON INBD SIDE OF STRINGER 28R AT BS 990. CLEANED AND EVALUATED AREA, NO CORROSION FOUND IAW SOPM 20-30-03 AND SRM 51-10-01.Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR 08FDEA01596Skin · dentedLWR FUSELAGE SKIN SURFACE DENT AT STR 21 L APPROX STA 1130. CUT OUT DAMAGED AREA DIM CUT OUT (4" X 1') IAW SRM 53-30-3 FAB REPAIR. TREATED AND PRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. TREATED AND PRIMED DOUBLEApr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA01595Skin · damagedLWR FUSELAGE STA 1125 6.5 INCHES RIGHT OF CENTER LINE SKIN HAS A PULLED THROUGH RIVET STR 29R. CUT-OUT DAMAGED AREA (DIMENSION 4" X 3") IAW SRM 51-10-1 & FABRICATED REPAIR DOUBLER & REPAIR FILLER IAW SRM 53-30-3 & 53-30-2 FIGURE 2, TREATED & PRIMED PARTS IAApr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA01594Angle · crackedVENTRAL STAIRWELL RT SIDE BELOW AIRSTAIR ACTUATOR FITTING, TORQUE BOX BS 1263 UPPER ANGLE FWD SIDE OF BULKHEAD HAS CRACK. REMOVED ANGLE FWD SIDE IAW SRM 51-30-2. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-30-5. INSTALLED NEW ANGLE IAW SRM 51-30-2.Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA01593Angle · crackedVENTRAL STAIRWELL RT SIDE BELOW AIRSTAIR ACTUATOR FITTING, TORQUE BOX BS 1263 UPPER ANGLE AFT SIDE OF BULKHEAD HAS CRACK. REMOVED UPPER ANGLE AFT SIDE IAW SRM 51-30-2. REMOVED WEB DOUBLER AND SEAL AND SEAL RETAINER FOR ACCESS IAW SRM 51-30-2. CUT OUT WEB DIM Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA01590Spar · crackedRT FALSE SPAR CRACKED JUST AFT OF NR 8 SPOILER FITTING. REPAIRED IAW DRAWING SR 27-57-038 REV C.Apr 25, 2008 · N203FE · Boeing 7272S2F · SpoilersSDR 08FDEA01589Skin · dentedRT LWR FUSELAGE SURFACE STA 1030 STA 1050, BELOW STR 26R HAS DENT. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREA , FABRICATED REPAIR DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3, TREATED AND PRIMED PARTS IAW SRM 51-30-2, INSTALLED COUNTERSINKApr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 08FDEA01588Web · crackedLT AIRSTAIR LOWER TORQUE BOX OUTER WEB CRACKED AT LIGHTING HOLE BS 1239. CUT OUT DAMAGE AREA DIM CUT OUT IAW SRM 51-10-1 AND 51-40-2. FAB REPAIR PARTS IAW SRM 51-40-2 & 53-10-2. TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED REPAIR PARTS IAW SRM 51-30-2.Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 08FDEA01586Frame · corrodedFWD PIT, FRAME AT STA 720D HAS CORROSION ON THE FWD FACE AROUND CABLE CUT OUT AT LBL 1. FOUND WITHIN LIMITS IAW SRM 53-10-2.Apr 25, 2008 · N203FE · Boeing 7272S2F · Fuselage Main, FrameSDR 08FDEA00646Wire Harness · burnedWHILE WORKING WRI 31-30/9464, TECH FOUND A SHORTED WIRE HARNESS IN AVIONICS COMPT. THE 3 PHASE WIRE HARNESS FROM THE EXTERNAL POWER RELAY HAS MADE CONTACT WITH GND BUS STRIP T268 (LOCATED DIRECTLY ABOVE APU GCU). INITIAL VISUAL INSPECTION SHOWS SEVERAL GND SFeb 26, 2008 · N213FE · Boeing 7272S2F · Electrical Power System WiringSDR 08FDEA00344Windshield · crackedAT FL310 PILOTS WINDSHIELD BEGAN TO CRACK ON INNER AND OUTER PANELS. REMOVED AND REPLACED CAPT'S WINDSHIELD IAW 727 MM 56-11-011-4. ALSO REPLACED WINDOW HEAT CONTROLLER IAW 30-41-033-4 AND 30-41-013-5. CHECKED WINDOW HEAT CONDUCTIVE COATING AND SENSOR PER MFeb 2, 2008 · N209FE · Boeing 7272S2F · Flight Compartment WindowsSDR 08FDEA00173Metering Valve · failedON TAXI IN OAK, TILLER WOULD NOT TURN TO THE LEFT, OK TO THE RIGHT. ALL HYD. PRESS GOOD. REMOVED AND REPLACED STEERING METERING VALVE IAW 727/200 MM 32-51-021-4. SYSTEM CKS NORMAL ALSO NO LEAKS. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 1692RA1Jan 16, 2008 · N201FE · Boeing 7272S2F · Steering Unit
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