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 06FDEA1960Duct · leakingON TAKEOFF LEG AT APPROX 500' AGL, NR 2 FIRE LIGHT ILLUMINATED AND FIRE WARNING BELL SOUNDED. ACCOMPLISHED RED TAB PROCEDURES. FIRELIGHT WENT OUT AFTER DISCHARGING ONE FIRE BOTTLE. INSPECTED NR 2 ENG IAW PW MM 72-00-00 FOR WINDMILLING. INSPECTED OIL FILTMay 17, 2006 · N217FE · Boeing 7272S2F · Engine (Turbine/Turboprop)SDR 06FDEA1444Indicator · malfunctionedREJECTED T/O AT 100 KTS 160,000 PDS. REQUIRES 33 MIN BRAKE COOLING FROM 0317Z. REJECT FOR CAPTAINS A/S INDICATOR. PERFORMED 33 MIN BRAKE COOLING INSP. CAPTAINS A/S INDICATOR CB PULLED BY MISTAKE FOR MEL 34-04-02. CB WAS RESET AND A/C RELEASED FOR SERVICE.Apr 13, 2006 · N205FE · Boeing 7272S2F · Airspeed/Mach IndicatorSDR 06FDEA1236Engine · leakingNR 2 OIL QTY DECREASED TO ZERO AT FLT LEVEL, APPROX 3 MIN LATER OIL PRESS DROPPED INTO YELLOW BAND AND CONTINUED TO FALL. COMPLIED WITH ALL RED TABS AND SHUTDOWN ENGINE. ENGINE WAS NEVER OPERATED AT ZERO OIL PRESSURE. WINDMILLED FOR APPROXIMATELY 15 MINUTESMar 26, 2006 · N212FE · Boeing 7272S2F · Turbine Engine Oil SystemSDR 06FDEA1118Position Switch · malfunctionedNR 2 L/E FLAP LIGHT REMAINED IN TRANSIT WHEN GOING FROM FLAPS 5 TO FLAPS 2. FOCUSING ON THE NR 2 KRUGER FLAP POSITION SW ADJ OR REPLACED. WILL REQUIRE RII SIGN-OFF. VERIFIED SWITCH GIVING BAD INDICATION, PARTS COMING FROM OUTSTATION. REMOVED AND REPLACEDMar 16, 2006 · N206FE · Boeing 7272S2F · Leading Edge Slat Position Indicating SystemSDR 06FDEA0629Control Unit · malfunctionedFWD CARGO SMOKE WARNING INFLIGHT, 15000 MSL. NO SMOKE IN COCKPIT. PHASE T'S ACCOMPLISHED. SYSTEM CHECKED GOOD AFTER LIGHT WENT OUT 30 SECONDS AFTER WARNING. RTB MEM. REMOVED AND REPLACED 4 EACH SMOKE DETECTOR UNITS FWD B/B IAW B727 AMM 26-17- 011-2. REMFeb 9, 2006 · N207FE · Boeing 7272S2F · Smoke DetectionSDR 06FDEA0547Fuel Control · malfunctionedNO THROTTLE RESPONSE ON NR 1 ENGINE ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL IAW FX B 727-200 MM 73-20-001-2. PERFORMED ENGINE RUN AND TRIM MED IAW FX B727-200 MM 71-00-030 AND 71-00-097 AND OPS AND LEAK CHECK GOOD. ALSO REMOVED AND REPLACEFeb 6, 2006 · N216FE · Boeing 7272S2F · Fuel Control/Turbine EnginesSDR 05FDEA04315Unknown · ground damageAIRCRAFT DAMAGED ON PUSHBACK, ON BELLY. REPAIRED AND INSPECTED.Dec 14, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, StructureSDR 05FDEA04115O-Ring · damagedREJECTED FIRST T/O DUE TO ENG FAIL LIGHT ON, NR 3 ENG ADV UP TO RED LINE N1 BUT EPR WAS STILL VERY LOW TO CONTINUE T/O, PILOT SAID ENG RED LINE NI WAS NOT EXCEEDED, REMOVED NR 3 ENG BULLET, PRESS TESTED THAT SECTION OF PT2 LINE, CHKS GOOD. FOUND THE TWO O-RINDec 4, 2005 · N217FE · Boeing 7272S2F · Power Indicating SystemSDR 05FDEA03901Cabin Pressure · malfunctionedDEPARTING GTF A/C WOULDN'T PRESSURIZE. AUTO FAIL AND STBY. LIGHTS NOT ILLUMINATED. RAN FAILURE OF PRESS. CONTROL CHECKLIST, MANUALLY CLOSED OUTFLOW VALVE AND RECYCLED PACK SWITCHES TO EVENTUALLY RESTORE PRESSURIZATION. NO DOOR LIGHTS ILLUMINATED BUT LOUD Nov 18, 2005 · N208FE · Boeing 7272S2F · Cabin Pressure Control SystemSDR 05FDEA03757Repair · undamagedFOUND REPAIR STA 500-520 LT BOTTOM FUSELAGE SKIN, BELOW MAIN CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT FS 500-FS520 S24L-S25L WAS DETERMINED TO Nov 10, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 05FDEA03756Repair · undamagedFOUND REPAIR RT INBD FORE FLAP. LEADING EDGE REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA, PREVIOUSLY INSTALLED REPAIR AT RT INBD FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1. Nov 10, 2005 · N213FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA03755Repair · undamagedFOUND REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE WAS DETERMINED Nov 10, 2005 · N213FE · Boeing 7272S2F · Wing Main, Frame StructureSDR 05FDEA03754Repair · damagedFOUND REPAIR LT I/B FORE FLAP, L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT I/B, FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1. BASED ON AN ENov 10, 2005 · N213FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA03758Repair · undamagedFOUND REPAIR TOP SIDE NR 3 L/E KRUGER FLAP LT WING. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 3 L/E KRUGER FLAP, TOP SIDE ON LT WING WAS DETERMINED TNov 10, 2005 · N213FE · Boeing 7272S2F · Leading Edge DevicesSDR 05FDEA03746Repair · undamagedFOUND REPAIR AFT CARGO COMPARTMENT STA 1010 RBL 8, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1010, RBL 8 WAS DETERMINED TO BE IAW SRM 51-40-4-FIG 1, BASENov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, StructureSDR 05FDEA03745Skin · undamagedFOUND REPAIR FORWARD CARGO COMPARTMENT, STA. 560- STA 620 RBL 20. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 560 STA 620 RBL 20 WAS DETERMINED TO BNov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 05FDEA03744Stringer · undamagedFOUND REPAIR AT STA 1030, RT SIDE OF FUSELAGE AT CUSP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT FS STA 1030 RT S 17R WAS DETERMINED TO BE IAW SRM 53-30Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Longeron/StringerSDR 05FDEA03743Skin · undamagedFOUND REPAIR AFT CARGO COMPARTMENT STA 1135 RBL 8, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1135 RBL 8 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 SHT 1 Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 05FDEA03741Skin · undamagedFOUND REPAIR AFT, CARGO COMPARTMENT STA 1105, RBL 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1105, RBL 5 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 BANov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 05FDEA03740Skin · undamagedFOUND REPAIR AFT CARGO COMPARTMENT STA 1080, LBL3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1080 LBL 3 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 BASEDNov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 05FDEA03644Floorbeam · corrodedLATERAL / LONGITUDINAL FLOORBEAM HAS SEVERAL CORRODED NUT PLATES AND SURFACE UNDER NUT PLATES ,FROM STA. 1090 TO 1110 BL 0 TO RBL 15., REMOVED CORROSION ON LWR. CHORD .090 BEFORE REWORK .040AFTER REWORK OUT OF LIMITS. IAW SRM 53-10-1. REMOVED CORRODED NNov 4, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 05FDEA03617Skin · dentedEXTERNAL FUSELAGE SKIN DENTED BS 1050 S-17R. CHECKED LIMITS MEASURED DENT .900 WIDE .750 LONG AND .055 DEEP A/Y =13.6 OUT OF LIMITS IAW SRM 53-10-1 FIG 1 SHEET 3 DETAIL II. NDT PERFORMED NO CRACK NOTED, FABRICATED DOUBLER AND CUT OUT DAMAGE. INSTALLED DOUNov 4, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 05FDEA03514Flap Track · corrodedNR 3 FLAP TRACK AFT MOUNT PAD HAS HEAVY CORROSION. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.Oct 26, 2005 · N213FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA03513Flap Track · corrodedNR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.Oct 26, 2005 · N213FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA03512Flap Track · corrodedNR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.Oct 26, 2005 · N213FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA03484Floorbeam · corrodedMDCC - FLOORBEAM BS 344 LBL-14-40 HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-6, BEFORE REMOVED MATERIAL 0.110 AFTER 0.104 WITHIN LIMITS IAW SRM 51-10-1. TREATED AND PRIMED IAW SRM 51-10-2.Oct 24, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 05FDEA03483Floorbeam · corrodedMDCC - FLOORBEAM CORRODED BS 312 LBL-42. REMOVED CORROSION IAW SRM 53-10- 1 MATERIAL LOSS OF 0.007 ORIGINAL THICKNESS 0.080 , FOUND TO BE WITHIN LIMITS PER SRM 53-10-1 FIG 5. TREATED AND PRIMED AREA IAW SRM 51-10-2.Oct 24, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 05FDEA03482Floorbeam · corrodedMDCC - FLOORBEAM BS 560 LBL21 HAS CORROSION. REMOVED CORROSION IAW SRM 53-10-1MAT LOSS OF .001 ORIGINAL THICKNESS OF 0.230 FOUND TO BE WITHIN LIMITS IAW SRM 51-10-6 TREATED AND PRIMED IAW SRM 51-10-2.Oct 24, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 05FDEA03447Beam · damagedCOMPLY WITH EA 7-5230-92344, DOORS, MAIN CARGO DOOR LOWER BEAM REPAIR AT BS 500.0. COMPLIED WITH EA 7-5230-92344 DOORS, MAIN CARGO DOOR LOWER BEAM REPAIR AT BS 500.Oct 18, 2005 · N211FE · Boeing 7272S2F · Fuselage Main, StructureSDR 05FDEA03160Switch · failedGOT AMBER LE FLAP LT ON FLAP RETRACTION AT FLAP 2 DEGREE SETTING. LE FLAP ANNUNCIATOR ON S/O PANEL SHOWED NR 6 IN TRANSIT. FOLLOWED QRH PROCEDURES, NO HELP RETURNED TO DEPARTURE AIRPORT. REMOVED AND REPLACED NR 6 L/E FLAP SWITCH PER MM 27-82-001-4. DURINGSep 29, 2005 · N203FE · Boeing 7272S2F · Leading Edge Slat Control SystemSDR 05FDEA03086Channel · corrodedMCD FLOOR SUPPORT SEVERAL NUT PLATES CORRODED BETWEEN STA 1130 TO STA 1148, RBL 27 TO RBL 62. REMOVED CORRODED FLOOR SUPPORT IAW SRM 51-30-2-1, FOUND OUT OF LIMITS IAW SRM 52-10-1 FIG 1. RECEIVED NEW FLOOR SUPPORT ON TRAV NR T5/547544, MAT ID 60357/7075-T651Sep 24, 2005 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 05FDEA03023Flap Track · corrodedNR 2 FLAP TRACK FWD MOUNT FITTING CORRODED AROUND BUSHINGS. REMOVED AND REPLACED NR 2 FLAP TRACK ASSY IAW MM 27-51-031-4.Sep 20, 2005 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA03019Floor Support · corrodedMAIN DECK FLOOR SUPPORT AT STA 852 BETWEEN LBL 45.50 AND 62, CORROSION UNDER CLIP NUT HOLES AND MOUNT BOLT AT LBL 45.5. REMOVED CORROSION IAW SRM 51-10-6, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED CHANNEL IAW 51-30-2. FABED NEW UPPER CAP USING MAT.Sep 20, 2005 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 05FDEA02998Flap Track · corrodedRT WING O/B FLAP I/B TRACK NR 7 HAS SURFACE CORROSION AND SMALL CHAFINGS ON FACES AND ROLLERS SLIDING TRACKS. REMOVED AND REPLACED FLAP TRACK IAW MM 27-51-032-4.Sep 19, 2005 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA02980Skin · crackedFUSELAGE SKIN IS DAMAGED, POSSIBLY CRACKED AT FS 190, AT APPROX 7 O'CLOCK POSITION, (NO STRINGERS IN THIS AREA.) MAJOR REPAIR PERFORMED HFEC IAW PTGNTM 51-00-00 CRACKED INDICATED AS MARKED. REMOVED DAMAGE IAW SRM 53-30-1FIG 1. FABRICATED REPAIR DOUBLER FROMSep 17, 2005 · N211FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 05FDEA02979Flap Track · corrodedRT WING OUTBD FLAP, OUTBD TRACK HAS SURFACE CORROSION AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REMOVED AND REPLACED NR 8 FLAP TRACK IAW MM 27-51-031-4.Sep 16, 2005 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA02978Flap Track · corrodedRT WING INBD FLAP OUTBD TRACK NR 6 HAS CORROSION, PITTING, AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REPLACED NR 6 FLAP TRACK ASSY IAW MM 27-51-031-4.Sep 16, 2005 · N211FE · Boeing 7272S2F · Trailing Edge FlapsSDR 05FDEA02814Gusset · crackedFWD CARGO DOOR AFT LOWER GUSSET IS CRACKED. REMOVED AND REPLACED GUSSET IAW SRM 51-30-2.Sep 8, 2005 · N211FE · Boeing 7272S2F · Cargo/Baggage DoorsSDR 05FDEA02813Gusset · crackedFWD CARGO DOOR GUSSET IS CRACKED AFT SIDE 3RD BRKT FROM TOP OF DOOR. REMOVED AND REPLACED GUSSET IAW SRM 51-30-2.Sep 8, 2005 · N211FE · Boeing 7272S2F · Cargo/Baggage DoorsSDR 05FDEA02784Indicator · malfunctionedREJECTED TAKEOFF UNDER 70 KNOTS DUE TO NO INDICATION ON NR 3 EPR GAUGE. COMPLIED WITH QRH AND MEL 77-01-01 NR 3 EPR INOP PROCEDURES. SUBSEQUENT TAKEOFF WAS UNEVENTFUL. PURGED MOISTURE FROM PT2 AND PT7 LINES TO NR 3 EPR TRANSMITTER WITH DRY NITROGEN AND RAN Sep 6, 2005 · N205FE · Boeing 7272S2F · Power Indicating SystemSDR 05FDEA02783Indicator · malfunctionedWHILE ADVANCING THROTTLES FOR T/O, NR 3 EPR INDICATOR JUMPED UP TO FROZE AT "2.07" AND REMAINED THERE FOR 5 MIN AFTER RTO WITH NR 3 THROTTLE AT IDLE. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01. NR 3 ENGINE EPR INDICATOR INOP. REMOVED AND REPLACED NR 3 ENG "Sep 6, 2005 · N208FE · Boeing 7272S2F · Power Indicating SystemSDR 05FDEA02730Switch · damagedAFTER T/O DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG AMBER LED LIGHT REMAINED ILLUMINATED S/O AUX PAN INDICATED NR 5 REMAINED EXT. PERFORMED QRH PROC AND LIGHT REMAINED ILLUM. RET TO LAND. REMOVED AND REPLACED NR 5 KRUEGER FLAP SWITCH AND STRAIGHTENED SWITCAug 31, 2005 · N201FE · Boeing 7272S2F · Leading Edge Slat Control SystemSDR 05FDEA02688Warning Light · illuminatedJUST AT BRAKE RELEASE AN "AFT AIRSTAIR" LIGHT ILLUMINATED. TAKEOFF WAS REJECTED. RTO CHECKLIST WAS ACCOMPLISHED. REJECTED TAKEOFF PARAMETERS, AIRSPEED <50 KIAS, EPR NR 1 NR 3 1.83, NR 2 1.75. TAKEOFF TIME 02:18. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. Aug 26, 2005 · N209FE · Boeing 7272S2F · Entrance StairsSDR 05FDEA02424Window · delaminatedUPPER PORTION OF WINDOW R1 IS DELAMINATING, AND A BUBBLING FLUID IS PRESENT INSIDE THE DELAM, R1 OUTER PANE CRACKED. REMOVED AND REPLACED RT NR 1 WINDSHIELD PER MM 56-11-011-4. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM 30-41-02, PRECAUTIONARY R/I.Aug 11, 2005 · N204FE · Boeing 7272S2F · Flight Compartment WindowsSDR 05FDEA02124Pump · failedHYD SYS B OVERHEAT LIGHT IN FLT TURNED ELEC PUMP NR 1 OFF AND LIGHT WENT OUT. REMOVED AND REPLACED NR 1 B PUMP PER MM-29-12-011-2. OPS CKS AND LEAK CKS GOOD. CYCLED ALL FLIGHT CONTROLS ON B SYS TO ENSURE NO AIR IN SYSTEM. NOTE, CASE DRAIN ALSO REMOVED AND Jul 28, 2005 · N204FE · Boeing 7272S2F · Hydraulic Pump (Electric/Engine), MainSDR 05FDEA01866Flap · jammedASYMETRICAL INBOARD TRAILING EDGE FLAPS AT 2 DEGREES UPON FLAP RETRACTION. RAN APPROPRIATE QRH PROCEDURES, FOUND LT INBD FLAP COCKED AND JAMMED INTO INBD AILERON. UPON FURTHER TROUBLESHOOTING FOUND BEARING WALKED OUT OF SCREWSHAFT END OF LT INBD TRANSMISSION.Jul 8, 2005 · N204FE · Boeing 7272S2F · Trailing Edge Flap Control SystemSDR 05FDEA01688Floor Support · crackedMAIN DECK BELOW FLOOR FS 1183 L-ANGLE CRACKED RBL 55, REMOVED L-ANGLE DITCHING SEAL, SEAL SUPPORT AND LT AND RT ANGLES IAW SRM 51-30-2. FABRICATED SEALS SUPPORT IAW DWG 65-29548. LOCATED, DRILLED AND INSTALLED PARTS IAW SRM 51-30-5 AND 51-30-2 MINOR REPAIR.Jun 26, 2005 · N203FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 05FDEA01663Antenna · corrodedNR 2 ADF ANTENNA DISBONDED AND CORRODED. REMOVED AND REPLACED NR 2 ADF LOOP ANTENNA IAW 34-37-012-4. PERFORMED OP CHECK IAW MM 34-37-001-5. OPS CHECKS GOOD.Jun 23, 2005 · N203FE · Boeing 7272S2F · Automatic Direction Finder (ADF) SystemSDR 05FDEA01662Angle · crackedNR 2 SPOILER UPPER SURFACE CRACKED AT 2 CENTER ATTACHMENTS. REMOVED AND REPLACED LT NR 2 SPOILER HINGE CUTOUT ANGLE IAW SRM 51-30-2.Jun 23, 2005 · N203FE · Boeing 7272S2F · SpoilersSDR 05FDEA01661Handle · crackedLT FWD EMERGENCY EXIT LOWER HANDLE ESCATION IS CRACKED. REMOVED AND REPLACED HANDLE ASSY IAW SRM 51-30-2. (M)Jun 23, 2005 · N203FE · Boeing 7272S2F · Emergency Exits
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