Boeing 727-247

Service difficulty reports · 2,669

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727247'
  ORDER BY difficulty_date DESC"

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SDR DL72W000581Frame · crackedTHE INNER CHORD OF THE C2 DOOR CUTOUT AFT FRAME AT FS 990 WAS FOUND WITH A .75 INCH CRACK IN THE HORIZONTAL FLANGE BETWEEN STRINGER 26R & 27R. THE CRACK WAS NEAR AN EXISTING CHORD REPAIR. THE EXISTING REPAIR WAS REMOVED AND A 4 INCH LONG SECTION OF HORIZONTMar 24, 2000 · N2812W · Boeing 727247 · Fuselage Main, FrameSDR DL72W000561Transceiver · inoperativeNR 2 NAV INOP, SPECIFICALLY NR 2 VOR, LOC AND GS INOP. AND OFF FLAG IN VIEW. DME WORKS NORMALLY. NAV TUNED TO MULTIPLE FREQUENCIES AT VARIOUS DISTANCE BUT EQUIP STILL UNRELIABLE. REPLACED XCVR ATTENUATE TO-60 ON VOR -50 ON ILS, OPS CK NORMAL.Mar 22, 2000 · N294WA · Boeing 727247 · Flight Environment DataSDR 00FDEA00162Skin · corrodedOUTER SKIN BULGING AND POPPED FASTENER HEADS BS 950F+13, STR 28L. ** S/D ** R&R DAMAGE PER FEDEX SRM 53-10-3 FIG 1.Mar 17, 2000 · N235FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W000593Splice · corrodedFOUND DURING MV2 CORROSION VISIT, CORROSION ON STRINGER 29 LT STRINGER SPLICE REPAIR DOUBLER STA 978 O/B SIDE AND STA 970 I/B (MARKED). REPLACED EXISTING REPAIR SPLICE ANGLES PER SRM 53-10-11D FIG 802D.Mar 17, 2000 · N293WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W000647Bracket · crackedFOUND AT MV2 CHECK, NR 7 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED AT LWR END. REPAIR PER M/M 57-42-0.Mar 16, 2000 · N293WA · Boeing 727247 · Leading Edge DevicesSDR DL72W000576Angle · crackedFOUND DURING MV2 CORROSION VISIT, LOWER COVE SKIN ATTACH ANGLE CRACKED ON NR 8 SLAT AT O/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812. NR 8 L/E SLAT (S/N BN 390).Mar 16, 2000 · N293WA · Boeing 727247 · Wing Miscellaneous StructureSDR 00FDEA00148Stringer · corrodedCORROSION (C53-113-01(1)) ON STRINGER AT RBL 15, WL 150, BS 674. ** S/D ** R&R PER FEDEX SRM 53-10-1, 53-10-3.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 00FDEA00150Skin · gougedEXTERIOR SECTION 48, HAS A GOUGE IN SKIN ATBS 1327 21 INCHES ABOVE AFT AIRSTAIR RT CUTOUT & DENT EXTEND APPROX 6 IN. AFT ** S/D ** REMOVED DAMAGE & FAB PER FEDEX SRM 53-30-3 FIG 1 & 53-30-1.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 00FDEA00153Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM AT BS 1110, LBL 4 TO LBL 11, WL 208 (C53-224-01). ** S/D ** R&R DAMAGE AREA PER IAW FEDEX SRM 53-10-08.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 00FDEA00152Intercostal · corrodedNR 1025 CORROSION ON INTERCOSTAL FLOOR SUPPORT AT BS 1105, RBL 11.5, WL 208 ( C53-224-01). ** S/D ** FAB, ALODINED & PRIMED INSTALL PER FEDEX SRM 51-10-1, 51-30-5, 51-30-6 AND 51-10-2.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 00FDEA00149Floorbeam · corrodedCORROSION (71C709-02) OF MAIN DECK FLOOR SUPPORT BEAM BETWEEN BS 1100 TO BS 1130, RBL 12, WL 208. VARIOUS LOCATIONS MARKED. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-6, 51-10-2, 51-20-1, 53-10-2.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 00FDEA00154Seat Track · corrodedCORROSION C53-224-01 ON SEAT TRACK BS 740-690, RBL 45, WL 208.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00151Skin · chafedNR 300 - SKIN CHAFED AT BS 720D+12.5 AT STR 19 LT. REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 14. FILLET SEALED PER FEDEX SRM 51-20-4.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 00FDEA00147Skin · chafedSKIN CHAFFED AT BS 720D PLUS 13 AT STR 20R.Mar 14, 2000 · N235FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W000503Hinge · corrodedTHE I/B LUG OF THE HORIZONTAL STABILIZER PIVOT HINGE AT LBL 10 WAS FOUND WITH CORROSION IN THE HOLE BORE AND ON THE I/B FACE OF THE LUG. THE BORE WAS OVERSIZED AND THE FACE LIGHTLY SPOTFACED TO REMOVE THE CORROSION. THE LUG WAS REPAIRED WITH A REPAIR BUMar 11, 2000 · N291WA · Boeing 727247 · Horizontal Stabilizer StructureSDR DL72W000320Battery · dischargedRIGHT OVERWING EMERGENCY EXIT LIGHTS FLASHING. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERIES.Feb 15, 2000 · N2819W · Boeing 727247 · Emergency LightingSDR DL72E000303Hinge · noiseyUPON LEVELING FL 260 LOUD PIERCING SQUEAL FROM FWD ENTRY DOOR. RAISED CABIN ALTITUDE, LOWERED CABIN ALT, CLIMBED A/C AND DESCENDED A/C. CABIN 5600 TO 1000 FT. A/C FL310 TO FL240. NO IMPROVEMENT. SQUEAL REMAINED. FOUND UPPER HINGE SEAL OUT OF PLACE. INSTFeb 13, 2000 · N282WA · Boeing 727247 · Passenger/Crew DoorsSDR UPS00231515Stringer · crackedINSPECTION TYPE:C, STR 1 BS 620, HOLE CRACKED AT REMOVED STRINGER CLIP LOCATION. REPAIRED STRINGER PER SRM.Feb 3, 2000 · N210UP · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 00FDEA00052Actuator · leakingAS FLAPS RETRACT AIR LIGHT FLICKERED ALONG WITH A SYS LOW PRESS LIGHT, THEN CAME ON STEADY. LOSS OF A SYS HYD LEFT NR 2 LEAD EDGE DEVICE FAIL. NR 2 KRUGER FLAP ACTUATOR LEAKING. *S/D* REMOVED AND REPLACED NR 2 LEAD EDGE ACT PER 727-200 MM 27-81-022-4.Feb 3, 2000 · N237FE · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72E000242Charger · inoperativeEMERGENCY LIGHT ON AFT CARGO DOOR INOP. REPLACED BATTERY CHARGER.Feb 1, 2000 · N283WA · Boeing 727247 · Emergency LightingSDR DL72W000222Smoke Detector · malfunctionedLAV SMOKE LIGHT ON S/O PANEL CAME ON INTERMITTENTLY DURING CLIMBOUT WITH NO INDICATIONS OF SMOKE. REPEAT WRITEUP. REPLACED LAV SMOKE DETECTOR.Jan 29, 2000 · N295WA · Boeing 727247 · Fire DetectionSDR DL72W000199Skin · crackedTHE UPPER FUSELAGE SKIN WAS FOUND WITH CRACK INDICATIONS AT THE UPPER ROW OF FASTENERS IN THE STRINGER 26R SKIN LAP SPLICE AT FS 662. ALL CRACK DAMAGE WAS REMOVED WITH A 4.25 X 2.75 CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER B727 Jan 26, 2000 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR UPS00231387Frame · corrodedINSPECTION TYPE:C, WHILE WORKING NRC 051193, FOUND CORROSION ON FRAME BS 600, RBL 8 WL 153. REPAIRED FRAMED PER SRM 53-10-2, 53-10-4, 51-30-2, MM 51-20-131.Jan 16, 2000 · N210UP · Boeing 727247 · Fuselage Main, FrameSDR UPS00231380Stringer Clip · crackedINSPECTION TYPE:C STRINGER CLIP CRACKED AT BS 660 STR5L AND STR 7L. REPLACED STRINGER CLIPS IAW SRM 51-30-2.Jan 14, 2000 · N210UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS00231390Stringer · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON STR28R BS 565 WL 148 RBL 8. REPAIRED STRINGER IAW SRM'S 53-10-3, 51-30-05, 51-30-2, MM 51-20-151 AND SRM 51-20-4.Jan 13, 2000 · N210UP · Boeing 727247 · Fuselage Main, Longeron/StringerSDR UPS00231389Web · corrodedINSPECTION TYPE:C CORROSION (C53-113-01.00-01), WEB BS560-580 WL 148 RBL 8. REPAIRED PER SRM'S 51-10-3, 51-30-5, 51-30-6, 51-20-4, 51-30-2.Jan 13, 2000 · N210UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS00231388Skin · corrodedINSPECTION TYPE:C, WHILE WORKING NRC 051378 (WINGS 75), FOUND CORROSION TO BE OUT OF LIMITS ON NR 3 K-FLAP. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.Jan 13, 2000 · N210UP · Boeing 727247 · Leading Edge DevicesSDR UPS00231386Skin · crackedINSPECTION TYPE:C, NR 4 SLAT UPPER SURFACE SKIN IS CRACKED AT O/B GUIDEHOOK UPPER FASTENER. REPAIRED PER SRM 57-50-3 FIG 10.Jan 12, 2000 · N210UP · Boeing 727247 · Leading Edge DevicesSDR DL72E000198Skin · bentI/B END, UPPER SKIN BENT. REPAIRED PER MM 57-52-0 FIG 803.Jan 1, 2000 · N831WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W992766Rib · crackedNR 12 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0 FIG 804.Dec 16, 1999 · N2811W · Boeing 727247 · Leading Edge DevicesSDR DL72W992765Rib · crackedNR 11 RIB CRACKED. REPAIRED PER M/M 57-54-0 FIG 804.Dec 16, 1999 · N2811W · Boeing 727247 · Leading Edge DevicesSDR DL72W992728Radar · failedAIRBORNE THE RADAR WOULD NOT PAINT ANY GROUND OR WX, BUT WOULD OCCASIONALLY SPIKE. REPLACED RT UNIT.Dec 13, 1999 · N296WA · Boeing 727247 · Independent Position Determining SystemSDR DL72E992731Web · crackedA .25 INCH CRACK AT LT TORQUE BOX VERT WEB LWR LIGHTENING HOLE STA 1233. TWO .1875 INCH CRACKS AT LT TORQUE BOX VERT WEB UPPER LIGHTENING HOLE STA 1223. BOTH REPAIRED PER MM 53-11-0.Dec 13, 1999 · N830WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E992730Web · crackedTWO CRACKS AT LIGHTENING HOLES RT TORQUE BOX VERT WEB STA 1223 AT UPPER LIGHTENING HOLE AND STA 1233 AT LOWER LIGHTENING HOLE. REPAIRED PER MM 53-11-0.Dec 13, 1999 · N830WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W992703Skin · corrodedTHE FUSELAGE SKIN BELOW THE LAVATORY SERVICE PANEL WAS FOUND WITH AN AREA OF SKIN CORROSION AT STRINGER 20R BETWEEN FS 300 & FS 312. THE CORROSION WAS REMOVED WITH AN 8 X 2 SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A Dec 9, 1999 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E992694Bracket · crackedNR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER MM 57-20-21.Dec 9, 1999 · N283WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992693Sensor · failedDURING CRUISE AT FL 290, A PASSENGER NOTICED THE AREA APPROXIMATELY 10 INCHES BELOW THE WINDOWS AT SEATS 16E & 17E WAS HOT TO THE TOUCH AND A SLIGHT BURNING ODOR WAS PRESENT. AFTER RT PACK TURNED OFF AND DESCENDED TO FL240, THE AREA COOLED IMMEDIATELY AND ODODec 9, 1999 · N831WA · Boeing 727247 · Cabin Pressure IndicatorSDR DL72E992691Angle · crackedDOUBLER CRACKED AT NR 2 L/E SLAT COVE SKIN ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.Dec 9, 1999 · N283WA · Boeing 727247 · Leading Edge DevicesSDR DL72W992684Wire · brokenAFT AISLE EXIT LIGHT INOP. FOUND BROKEN WIRE AT CANNON PLUG. REMOVED AND REPLACED CANNON PLUG.Dec 8, 1999 · N290WA · Boeing 727247 · Light System WiringSDR DL72W992672Bracket · crackedNR 5 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED TOP AND BOTTOM RADIUS. REPAIRED PER MM 57-20-21.Dec 7, 1999 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W992662Valve · failedAT 37,000 FT CARGO VALVE LIGHT ON, UNABLE TO CONTROL CABIN ALTITUDE. REPLACED LT PACK FLOW CONTROL VALVE, OP CKS GOOD.Dec 7, 1999 · N290WA · Boeing 727247 · Cabin Cooling SystemSDR UPS99231183Battery · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHT AT MAIN ENTRY DOOR INOP. REPLACED BATTERIES, OPS CK GOOD.Dec 6, 1999 · N212UP · Boeing 727247 · Emergency LightingSDR DL72W992659Skin · delaminatedLTR CHK C-1 12/6/99, NR 3 SPOILER DELAMINATED UPPER O/B SIDE. REPAIRED PER SRM 57-50-6.Dec 6, 1999 · N2816W · Boeing 727247 · SpoilersSDR DL72W992649Light · inoperativeFWD AND AFT RT OVERWING EMERGENCY LIGHTS INOP. REPLACED RACK, OP CKS GOOD.Dec 4, 1999 · N296WA · Boeing 727247 · Emergency LightingSDR DL72E992645Actuator · failedAFTER TAKEOFF, NR 7 SLAT WOULD NOT RETRACT UNTIL BACK ON GROUND. REPLACED NR 7 SLAT ACTUATOR AND EXTEND SWITCH, CHECKS OK.Dec 4, 1999 · N831WA · Boeing 727247 · Trailing Edge Flap ActuatorSDR 99FDEA00493Unit · failedRT MLG IND UNSAFE ON EXTENSION. WHILE WORK CKLIST GEAR LATER WENT DOWN AND LOCKED IND FOR NO REASON. *S/D* REPLACED LAND GEAR ASSY BOX PRECAUTIONARY. OPER CK PER ENG AUTH 7-3209-4087-1 REVISION A AND MM 32-09-122-5 STEPS 5A-E.Dec 1, 1999 · N237FE · Boeing 727247 · Landing Gear Position and WarningSDR DL72W992627Coalescer · contaminatedSMOKE ENTERED CABIN AFTER START, PACKS WERE ON BUT NOT OVERHEATED. PNEUMATIC SOURCE WAS APU ON ENGINE NR 1. REPLACED APU FLOW-MULTIPLIER AND COALESCER BAGS. SERVICED APU TO PROPER LEVEL, OP CKS GOOD.Nov 30, 1999 · N2812W · Boeing 727247 · Humidity Control SystemSDR DL72W992623Light · inoperativeON PREFLIGHT CHECKLIST, CREW FOUND RIGHT REAR EMERGENCY OVERWING LIGHT INOP IN EMERGENCY MODE ON TEST. FOUND CANNON PLUG DISCONNECTED ON ASSOCIATED BATTERY PACK. RECONNECTED CANNON PLUG, LIGHT TESTS GOOD IN EMERGENCY MODE ON CHECK OUT.Nov 30, 1999 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W992604Engine · malfunctionedDURING T/O, NR 1 THROTTLE HAD TO BE ADVANCED BEYOND NORMAL POS TO ATTAIN T/O EPR, EGT AND N2 WERE IN CAUTION RANGE FOR NR 1 ENG & N1 WAS LOWER THAN NR 2 & NR 3 ENG. DUCT PRESS ON LT SIDE WAS 30 PSI ON RT 68 PSI. AFT F/A HEARD WHAT SOUNDED LIKE A BACKFIRE ONNov 23, 1999 · N2812W · Boeing 727247 · Engine (Turbine/Turboprop)SDR DL72W992589Stiffener · crackedL/E SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK I/B STIFFENER. REPLACED PER M/M 57-20-21 PG 813 {NR 6 SLAT}.Nov 23, 1999 · N2814W · Boeing 727247 · Leading Edge Devices
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