Boeing 727-2D4

Service difficulty reports · 279

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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 = '7272D4'
  ORDER BY difficulty_date DESC"

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SDR 01FDEA00764Coupling · leakingLWR AFT BODY OVERHEAT LIGHT ILLUM'D AFTER LEVEL OFF, ACCOMP'D RED TABS, RED TABS CONFIRMED NR 3 BLEED LEAK BET BLEED VALVE & PACK VALVE. REMOVED AND REPLACED COUPLING, SLEEVE, RING AND RETAINER PER SMP.Aug 22, 2001 · N287FE · Boeing 7272D4 · Pneumatic Distribution SystemSDR 01FDEA00753Frame · crackedUPPER FLANGE AT BS 640 FRAME IS CRACKED AT FLOOR SUPPORT ATTACH POINT AT RBL 2.5 & LBL 2.5 WL 155. REMOVED AND REPLACED PER SRM 51-40-3.Aug 18, 2001 · N288FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00754Frame · crackedBS 660 FRAME UPPER FLANGE CRACKED AT FLOOR SUPPORT ATTACH POINTS, RB. 8.5 WL 155. REMOVED AND REPLACED UPPER FLANGE PER SRM 51-40-3.Aug 18, 2001 · N288FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00752Splice · corrodedCORROSION (C53-113-01,1) ON STR 27R AT BS 482. REMOVED AND REPLACED SPLICE PER SRM 51-10-2, 51-20-4, 51-30-2.Aug 18, 2001 · N288FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 01FDEA00458Skin · corrodedBULGE IN EXT BELLY SKIN BS 950+5 INCH BL 0. REMOVED AND REPLACED PER FEDEX SRM 53-10-3 FIG 1, EA 7-5330-57281.Jun 18, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 01FDEA00463Stringer · corrodedCORROSION ON STR 28L, BS 700+15, WL 153. *S/D* REMOVED AND REPLACED STR PER IAW FEDEX SRM 53-10-1, 53-10-3.Jun 18, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, Longeron/StringerSDR 01FDEA00457Shear Tie · corrodedEXTERIOR SKIN BULGED BS 500 BETWEEN STR 25 & 26 RT. *S/D* REMOVED AND REPLACED CORRODED SHEAR TIE PER IAW FEDEX SRM 51-10-6, 51-30-2, FEDEX MM 51-20-191, 51-20-21.Jun 18, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, StructureSDR 01FDEA00456Frame · dentedFRAME IS DENTED AT BS 660 AT STRINGER 25 RT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-30-2, 51-40-3.Jun 18, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00455Frame · dentedFRAME IS DENTED AT BS 680 AT STRINGER 24 RT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-30-2, 51-40-3.Jun 18, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00464Skin · corrodedNR 703 BULGE EXTERIOR SKIN BS 950E+3, STR 28 LH. ** S/D ** R&R SKIN PER IAW FEDEX EA 7-5330-57274.Jun 18, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 01FDEA00454Stringer · crackedNR 838 WHILE WORKING N0301 FND CRACK EMANATING FROM OPEN HOLE AT BS 460, STR 3 L/H. ** S/D ** R&R STRING PER FEDEX SRM 53-10-3, 51-20-151, 53-10-3.Jun 18, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, StructureSDR 01FDEA00433Skin · damagedCREASE IN EXTERNAL SKIN AT BS 1193 JUST BELOW STR 16R. *S/D* REMOVED AND REPLACED SKIN PER FEDEX SRM 53-30-3 FIG 1.Jun 11, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 01FDEA00434Skin · corrodedBULGE IN EXTERIOR SKIN BS 700 JUST ABOVE STR 26 RT.Jun 11, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 01FDEA00432Frame · dentedFRAME IS DENTED AT BS 700 BETWEEN STR 23 RT AND 24 RT.Jun 11, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00431Frame · dentedFRAME DENTED TWO PLACES AT BS 500 BETWEEN STR 23 LT AND 25 LT.Jun 11, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00430Frame · dentedFRAME IS DENTED AT BS 600 BETWEEN STRINGER 23 LT & 24 LT.Jun 11, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00429Frame · dentedFRAME IS DENTED AT BS 560 AT STRINGER 24 LT.Jun 11, 2001 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 01FDEA00110Pressure Switch · false indicationON T/O, GLARESHIELD ENG FAIL AND MASTER WARNING LIGHT WITH BELL ILLUM. REMOVED AND REPLACED ALL 3 AUTO PACK TRIP SYS PRESSURE SWITCHES PER B727-200 MM 21-11-011-4. REPLACED F/O''S FIRE BELL RESET LIGHT ASSY PER SMP.Feb 11, 2001 · N287FE · Boeing 7272D4 · Detection SystemSDR 01FDEA00104Power Unit · malfunctionedT/O ROLL FIRE WARNING LIGHT CAME ON GLARESHIELD ILLUMINATED WITH ALARM BELL. REMOVED AND REPLACED APU FIRE AND OVERHEAT DET PWR UNIT PER IAW 727-200 MM 26-15-003-4 AS PRECAUTIONARY. SYS OPS CK NORMAL.Feb 9, 2001 · N287FE · Boeing 7272D4 · Fire DetectionSDR 01FDEA00021Link · corrodedAFT T/O DURING FLAP RETRACT BOTH INBOARD AND OUTBOARD TRAILING EDGE FLAP IND STOPPED. AMBER LIGHT ILLUM, BUT EDGE DEVICE SHOW ALL GREEN ON 2ND OFF PNL. *S/D* CLEAN, LUB JACKSCREWS, GIMBALS, ROD ENDS, PULLEYS, AND CABLES PER MM 12-22-001-2. REMOVED AND REPLJan 13, 2001 · N287FE · Boeing 7272D4 · Trailing Edge Flap Control SystemSDR 00FDEA00451Clamp · leakingLWR AFT BODY OVERHEAT LIGHT IN FLT. PERFORMED PROC ON 2-7-14 TO STEP 14, LIGHT WENT OUT. FOUND CLAMP ON PURGE AIRLINE TO AIR CLEANER IN LEFT AFT AIRSTAIRS LEAKING. TIGHTENED CLAMP PER STANDARD MAINT PRACTICES. RAN APU PER JET RUN HDBK, NO LEAKS NOTED.Jul 13, 2000 · N287FE · Boeing 7272D4 · Pneumatic Distribution SystemSDR 00FDEA00326Warning Light · illuminatedON T/O AT 400 ENG FAIL LIGHT FOLLOWED BY NR 2 FIRE LIGHT & BELL. FOLLOWED RED TABS WHICH IND BLD AIR LEAK. *S/D* REMOVED AND REPLACED 13TH STAGE MANIFOLD ASSY PER WORK CARD 7102-2010 PG 3 TASK 4. LEAK CK NORM. REPLACED MISSING BLOW OUT PNLS ON RIGHT COWLIMay 11, 2000 · N288FE · Boeing 7272D4 · Pneumatic Distribution SystemSDR 99FDEA00386Fire Light · illuminatedTHE 2 FIRE WARN BELL CUTOUT LIGHTS ILLUM. ALL ENG INSTRUMENTS AND IND WERE NORMAL. TESTED ALL ENGINE FIRE LOOPS PER 727 MM 26-11-001-0, ALL TEST NORM. RAN ALL ENG PER JET RUN HDBK, NO DEFECTS NOTED.Sep 15, 1999 · N287FE · Boeing 7272D4 · Fire DetectionSDR 99FDEA00065Angle · corrodedRT WING LWR SURFACE OF FRONT SPAR CHORD ANGLE HAS EXFOLIATED CORROSION AFT OF NR 5 L/E SLAT T DUCT. REMOVED CORROSION SPAR CHORD METAL. CORROSION BEYOND LIMITS (ORIG THICK 0.316 AFTER BLEND 0.0220). REPAIR STRAP INSTALLED ON UPPER SURFACE OF FRONT SPAR CHORFeb 17, 1999 · N288FE · Boeing 7272D4 · Wing Miscellaneous StructureSDR 99FDEA00064Floorbeam · corrodedUPPER LOBE, CORROSION FWD EDGE OF TOP FLANGE ON FLOORBEAM BS 1130, LBL 3 AND FLOORBEAM 1130, LBL 19 TOP FLANGE. REMOVED CORROSION WAS OUT OF LIMITS. INSTALLED FLOORBEAM REPAIR PER EA 7-5310-42947.Feb 17, 1999 · N288FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR 99FDEA00063Floorbeam · damagedTWO DOUBLE DRILL HOLES BS 1130, LBL 25, 30 AND DOUBLE DRILL HOLES BS 1148 AND 1166. REPAIRED DAMAGE TO FLOORBEAMS DUE TO DOUBLE DRILL HOLES PER EA 7-5310-42962. TREATED AND PRIMED PER 51-20-0.Feb 17, 1999 · N288FE · Boeing 7272D4 · Fuselage Main, Floor BeamSDR 99FDEA00062Stringer · gougedUPPER LOBE BS 440 STRINGER 8L TOP OF STRINGER GOUGED. BLENDED OUT GOUGE, OUT OF LIMITS. INSTALLED DOUBLER PER SRM 53-10-3 FIG 2.Feb 17, 1999 · N288FE · Boeing 7272D4 · Fuselage Main, Longeron/StringerSDR 98FDEA00728Switch · lack of lube98-295 - TAIL SKID LIGHT REMAIN ON AFT T/O, CYCLED THE LAND ONCE, LIGHT STILL ON. REMOVED AND REPLACED GEAR PINS. CLEAN AND LUBE TAIL SKID UP SWITCH. TAIL SKID IS FAIRED WITH FUSELAGE WHEN IN RETRACT POSITION.Dec 8, 1998 · N287FE · Boeing 7272D4 · Auxiliary Gear (Tail Skid)SDR 98FDEA00598Libht · inoperative98-238 ON INIT T/O, THE RT GEAR DOOR LIGHT REMAIN ILLUM. ACCOMPLISH RED TABS. LIGHT REMAIN ILLUMINATED, SUSP RIGHT GEAR DID NOT RETRACT. WITH GEAR DOWN ANTI-SKID INOP AND SYS 'A' QUANTITY 2.5 GAL. REMOVED ANTI-SKID CONTROL UNIT. REPLACED STRUT DOOR SUPPOSep 29, 1998 · N288FE · Boeing 7272D4 · Landing Gear Position and WarningSDR 98FDEA00584Accessory Box · failedCLIMBOUT, AC ELEV BUMPED IN LEFT TURN. AUTO PILOT SERVO IN AB. AFT LEVEL OF FLT LEVEL 310 ELEV TRIM RAN AWAY. AUTO PILOT DISCONN AND CRUISE CONT TO RUN. COULD NOT DUP PROBLEM. REMOVED AND REPLACED AUTO PILOT ACCY BOX PER MM 22-11-141 AND RELAY R102 AUTO PSep 18, 1998 · N287FE · Boeing 7272D4 · Autopilot SystemSDR 97FDEA00900Fuel Pump · failed97-0257 - NR1 ENGINE FAILURE AT 400 FEET ABOVE GROUND LEVEL. POP HEARD IN COCKPIT. ENGINE WINDMILLED WITH NORMAL INDICATIONS. RESTART UNSUCCESSFUL. FOUND INPUT SHAFT FOR FUEL PUMP SPLINES STRIPPED INSIDE PUMP. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PEDec 23, 1997 · N287FE · Boeing 7272D4 · Engine Fuel PumpSDR 97FDEA00770Lock Solenoid · failedLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. COMPLIED WITH CHECKLIST AND RETURNED TO BASE. FOUND LANDING GEAR LOCK SOLENOID BAD. REPLACED SOLENOID PER BOEING MAINTENANCE MANUAL 32-31-16. GEAR LEVER OPERATIONAL CHECK GOOD.Oct 21, 1997 · N288FE · Boeing 7272D4 · Landing Gear Retraction/Extension SystemSDR 97FDEA00766Bolt · failedAFTER TAKEOFF, LANDING LEVER WOULD NOT MOVE TO THE UP POSITION. FOLLOWED LANDING GEAR LEVER LATCH FAILS TO RELEASE CHECKLIST. MANUALLY RELEASED LANDING GEAR LEVER LATCH AND GEAR RETRACTED NORMALLY. REMOVED AND REPLACED BOLT IN LEFT MAIN LANDING GEAR ACTUATOOct 21, 1997 · N288FE · Boeing 7272D4 · Landing Gear Position and WarningSDR 97FDEA00308Gear Light · failed97-0095, WHEN GEAR SELECTED DOWN THE RIGHT MAIN LIGHT DID NOT COME ON. TEST WAS GOOD. THE DOOR OPENED WITH THE HANDLE. RECYCLED THE GEAR THREE TIMES AND IT FINALLY CAME ON. PHYSICALLY CHECKED WIRE CONNECTIONS AT DOWN LOCK SWITCH. COULD NOT FIND PROBLEM ORMay 24, 1997 · N287FE · Boeing 7272D4 · Landing Gear Position and WarningSDR 97FDEA00096Clamp Insulator · out of positionNR 1 FIRE DETECTOR CIRCUIT LIGHT ILLUMINATED IN-FLIGHT. THE FIRE WARNING TEST WAS INITIATED AND TESTED SUCCESSFULLY. ENGINE INSTRUMENTS APPEARED NORMAL. FOUND ONE CLAMP INSULATOR OUT OF POSITION. REPOSITIONED INSULATOR AND LOOP. LIGHT EXTINGUISHED WITH COFeb 9, 1997 · N288FE · Boeing 7272D4 · Fire DetectionSDR 96FDEA01439Gasper Fan · failedGASPER FAN INOPERATIVE. CIRCUIT BREAKER POPPED OUT 3 TO 4 SECONDS AFTER TURNING GASPER FAN ON, BAD SMELL CAME OUT OF THE GASPER SOCKETS. REMOVED AND REPLACED GASPER FAN PER B727 MAINTENANCE MANUAL 21-23-11, OPERATIONAL CHECK GOOD.Sep 6, 1996 · N287FE · Boeing 7272D4 · Air Distribution FanSDR 96FDEA01354Skin · corrodedNR0236 AND 011, CORROSION (71C208-02) FWD CARGO BAY SKIN AT BS 720C PLUS 13 JUST I/B OF STR 28L. *S/D* REPAIRED CORROSION DAMAGE IN FWD CARGO BAY SKIN AT BS 720C PLUS 3 IAW FEDEX SRM 53-30-3.Aug 13, 1996 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 96FDEA1328Skin · creasedNR0430 & 009 SHARP CREASE IN SKIN FROM STA 303 - 325 L/H BETWEEN STR 3-4. ****S/D***** REPAIRED CREASE IN SKIN PER FEDEX SRM 53-30-3. DAMAGED AT BS 303 BETWEEN STR 3 & 4L WAS REPAIRED ON NR-0471.Aug 7, 1996 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 96FDEA01341Gate · corrodedNR0486 & 010 WHILE WORKING NR0400 FOUND FWD ENTRY DOOR UPR GATE TO BE CORRODED SEVERELY. ****S/D**** R/R FWD ENTRY DOOR UPPER GATE. ALL WORK DONE IAW FEDEX SRM 51-30-2.Aug 6, 1996 · N288FE · Boeing 7272D4 · Passenger/Crew DoorsSDR 96FDEA01312Web · crackedNR0447 AND 008, WHILE ACCESSING WEB FOR REPAIR ON NR0052, FOUND WEB TO BE CRACKED AND CORRODED AT BS 294.5 TO 344 WL 170 RBL 34. *S/D* REMOVED CORROSION ON WEB AND FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED WEB, USING OLD WEB AS A TEMPLATE,Aug 5, 1996 · N288FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 96FDEA01310Skin · crackedNR0444 AND 007, AFT AIRSTAIR CUTOUT L/FWD CORNER CRACKED PAST RIVET BS 1220 STR 26. *S/D* REPAIRED CRACK AT BS 220 STR 26L IAW FEDEX STANDARD REWORK DRAWING SR 27-53-024.Aug 2, 1996 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/SkinSDR 96FDEA01308Stringer Clip · crackedFWD CARGO BAY STR CLIP HAS TORN EDGE BS 640 STR 27L. FABRICATED STR CLIP AND INSTALLED AT BS 640 STR 27L PER FEDEX SRM 53-10-1.Aug 1, 1996 · N288FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 96FDEA01303Shear Tie · corrodedNR 0141, 024 CORROSION (C53-1113-0141) IN THE FWD CARGO BAY ON FRAME SHEAR TIE BS 600 WL 150 RBL 17. *S/D* REMOVED CORRODED SHEAR TIE AT BS 600 WL 150 RBL 1. FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 600 WL 150 RBL 17 PER FEDEX SRM 53-10-4.Jul 31, 1996 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 96FDEA1298Doorway Frame · gougedNR 0419 005. RIGHT AFT EMERGENCY EXIT DOORWAY AFT FRAME IS GOUGED 1.5 INCHES LONG AT BS 848.95 RBL 69.5 WL 234 GOUGE IS IN RADIUS. REWORKED GOUGED AREA OF RT AFT EMERGENCY EXIT DOORWAY FRAME IAW FEDEX EA 7-5310-29767.Jul 30, 1996 · N288FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 96FDEA01299Skin · delaminatedNR 0028, 004 LEFT WING O/B FOREFLAP I/B END HAS A LARGE DELAMINATED TEMPORARY REPAIR. *S/D* LEFT WING O/B FOREFLAP I/B END WAS REPAIRED PER FEDEX SRM 51-40-6.Jul 30, 1996 · N288FE · Boeing 7272D4 · Trailing Edge Flap Control SystemSDR 96FDEA01311Bracket · crackedNR0360 AND 025, NR 1 ENG CONTROL QUADRANT SUPPORT CASTING CRACKED JUST FORWARD AND I/B OF THRUST CRACK. *S/D* REMOVED AND REPLACED NR 1 ENG CONTROL QUADRANT SUPPORT CASTING PER FEDEX MM 76-12-0, 71-21-22, 71-21-21, 78-30-15, 76-12-41 AND 71-00.Jul 29, 1996 · N287FE · Boeing 7272D4 · Engine ControlsSDR 96FDEA01291Frame · crackedNR 0386 023. FRAME IS CRACKED UNDER UPPER FLANGE AT STA 950E, 4.50 INCHES INBOARD OF STR 26L FROM HI-LOCK FASTENER HOLE INTO RADIUS OF FLANGE (OVER .25 INCH LONG). REMOVED DAMAGE AND REPAIRED FRAME UNDER UPPER FLANGE AT BS 950E, LBL 7 - 35 PER FEDEX SRM 51-4Jul 26, 1996 · N287FE · Boeing 7272D4 · Fuselage Main, FrameSDR 96FDEA01284Bonding Jumper · corrosionNR 0261 003. CORROSION AROUND NR 2 K-FLAP OUTBOARD LOWER BONDING JUMPER UPPER ATTACH POINT. REPAIRED NR 2 K-FLAP OUTBOARD LOWER BONDING JUMPER UPPER ATTACH POINT IAW SRM 57-50-03. MOVED ATTACH POINT IAW SRM 27-57-010C.Jul 24, 1996 · N288FE · Boeing 7272D4 · Leading Edge DevicesSDR 96FDEA01287Intercostal · corrodedNR 01148 022. CORROSION C53-113-01(1) IN THE FORWARD CARGO BAY ON INTERCOSTAL BS 720, WL 148, LBL 10. ****S/D***** COMING.Jul 23, 1996 · N287FE · Boeing 7272D4 · Fuselage Miscellaneous StructureSDR 96FDEA01280Chord · crackedDISCREPANCY: NR 0305 (21) CRACK IN PLUS CHORD AT BS 760, LBL 70.5, WL 205. CORRECTIVE ACTION: *****S/D *****COMING.Jul 22, 1996 · N287FE · Boeing 7272D4 · Wing Miscellaneous Structure
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