Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  ORDER BY difficulty_date DESC"

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SDR 05FDEA03050Wire · meltedWIRE BUNDLE MELTED TO LEFT AFT AIR CONDITIONING HEAT EXCHANGER AFT SIDE. REMOVED MELTED PLASTIC FROM HARNESS IAW BOEING SWPM 20-10-11. NO DAMAGE TO WIRING WAS FOUND. REPOSITIONED HARNESS AND INSTALLED PROTECTIVE SLEEVING IAW BOEING SWPM 20-10-11.Sep 22, 2005 · N267FE · Boeing 727233 · Air Conditioning System WiringSDR 05FDEA03048Connector · deterioratedON T/O FROM MSN, PLACED GEAR HANDLE TO UP, GEAR RETRACTED AND ALL LIGHTS EXTINGUSIHED NORMALLY, HOWEVER WHEN THE GEAR HANDLE WAS PLACED TO OFF, THE RED DOOR LIGHT ON FWD PANEL AND RT MAIN GEAR DOOR LIGHT ON S/O PANEL ILLUMINATED. REMOVED THE CANON PLUG FROMSep 22, 2005 · N265FE · Boeing 727233 · Landing Gear System WiringSDR 05FDEA03021Floorbeam · corrodedFLOORBEAM CORRODED STA 720A FROM BL0 TO LBL45. REMOVED, FABRICATED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR STA 720A BLO TO LBL 45 ALL IAW FX SR 27-53-034E FIG 5, FX B727 SRM 51-10-2, 53-10-1, BAC5619(H) AND BAC 5701.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03018Seat Track · corrodedSEAT TRACK CORRODED STA 690-740 AT LBL45. REMOVED SEAT TRACK, LOCATED AND DRILLED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK FROM STA 690 TO 740 AT LBL45 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03017Seat Track · corrodedSEAT TRACK CORRODED STA 690-740 AT LBL24. REMOVED SEAT TRACK, LOCATED AND DRILLED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK SECTION STA 690-740 AT LBL 24 ALL IAW FX B727 SRM 53-10-5, 51-30-2,51-10-5 AND 51-10-2.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03016Seat Track · corrodedSEAT TRACK CORRODED STA 480-690 AT LBL 24. REMOVED DAMAGED SEAT TRACK STA 480-690 AT LBL24, LOCATED AND DRILLED NEW SEAT TRACK, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK AT STA 480-690 AT LBL 24 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03020Floorbeam · corrodedFLOORBEAM CORRODED STA 480 FROM BL0 TO LBL45. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 480 FROM BL0 TO LBL45 ALL IAW FX B727 SRM 53-10-8, 53-10-1 AND 51-10-2.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03015Seat Track · corrodedSEAT TRACK CORRODED STA 720-740 AT BL0. REMOVED CORRODED SEAT TRACK AT STA 720-740 ON BL 0, LOCATED AND DRILLED NEW SEAT TRACK, ALODINED, PRIMED AND INST NEW SEAT TRACK SECTION STA 720-740 AT BL0 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03014Seat Track · corrodedSEAT TRACK CORRODED STA 480-690 AT LBL 45. REMOVED SEAT TRACK STA 480-690 AT LBL 45 IAW FX B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK AND SPLICES IAW FX B727 SRM 53-10-5. ALLODINED, PRIMED AND INSTALLED SEAT TRACK IAW FX B727 SRM 53-10-5, 51-30-2, Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03013Floorbeam · corrodedFLOORBEAM CORRODED STA 680 FROM BLO TO LBL 45. REMOVED CORROSION IAW FX B727 SRM 51-10-6. FOUND AREA FROM LBL8 TO LBL12 TO BE OUT OF LIMITS IAW FX P-F SRM 53-10-1. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW FX SR27-53-034E FIG 1. ALODINED AND PRIMSep 20, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03012Floorbeam · corrodedFLOORBEAM STA 322 CORRODED AT BL0TO LBL45. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW FXB727 SRM 53-10-8 FIG 9. ALODINED AND PRIMED PARTS IAW FX B727 SRM 51-10-2.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03011Floorbeam · corrodedFLOORBEAM STA 344 HAS CORROSION AT LBL10-RBL16 (PREVIOUS SPLICE AT LBL10). REMOVED DAMAGED AREA PER FE SR27-53-007 FIG 11. FABRICATED AND INSTALLED NEW UPPER CAP BEAM REPAIR IAW FX SR27-53-007 FIG 11. ALLODINED AND PRIMED IAW FX B727 SRM 51-10-02.Sep 20, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03009Floorbeam · corrodedFLOORBEAM CORRODED STA 560 FROM BL0 TO LBL45. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP IAW FX SR27-53-034E FIG 30 SHT 5. FABRICATED, DRILLED AND LOCATED REPAIR "T", SUPPORTS, FILLERS, ANGLES AND "T" CAP REPAIR ANGLES IAW FX SR27-53-034E FIG 30 SHT 5. INSTALSep 20, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA03008Indicator · inoperativeCAPTAINS AIRSPEED INDICATOR DID NOT INDICATE AIRSPEED ON T/O. ACN RELEASED FOR SERVICE PER MEL/CDL: 20-01 CATEGORY: X RVSM ITEM "MEL 20-01: DO NOT OPERATE AIRCRAFT WITHIN RVSM AIRSPACE." "NO RVSM OPERATIONS". R/R CADC PER M/M 34-12-011-4, OPS CHECK GOOD. DESep 20, 2005 · N254FE · Boeing 727233 · Airspeed/Mach IndicatorSDR 05FDEA03006Display · inoperativeAFTER T/O, SWITCHING FROM TERRAIN TO WX MODE OR RADAR, LOST RANGE MARKER AND DATA DISPLAY. ACTUAL WX RETURNS WORKED. REMOVED AND REPLACED INDICATOR R/T AS PRECAUTIONARY. REF B727-200MM SEC 34-41-031-4 AND 34-41-041-4.Sep 20, 2005 · N222FE · Boeing 727233 · Weather Radar SystemSDR 05FDEA02953Skin · damagedWHILE WORKING N00667, FOUND EXTERNAL SKIN REPAIR AT BS 1191 - 1203 AT STR 23 RT TO HAVE INSUFFICIENT ROWS OF FASTENERS AT UPPER AFT CORNER OF REPAIR DOUBLER. REPAIRED PER SRM 53-30-3.Sep 16, 2005 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA02898Floorbeam · misdrilledFLOORBEAM STATION 380 HAS PREVIOUS DRILLED HOLES IN RADIUS AND NO EDGE DISTANCE AT LEFT BUTT LINE 50 TO 60. CUT OUT DAMAGE SECTION OF UPPER BEAM CAP IAW FEDEX SR27-53-034E FIGURE 30. REMOVED TIEDOWN, RADIUS STOPS AND VERTICAL STIFFENERS IAW FEDEX SRM 51-30Sep 14, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA02893Floorbeam · corrodedFLOORBEAM CORRODED STA 720D FROM RBL 24 TO LBL 45. REMOVED, FABBED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 720D FROM RBL 24 TO LBL 45 ALL IAW FX SR27-53-034E FIG. 1 & 4, FX B727 SRM 51-10-2, BAC5619 (H) AND BAC 5701.Sep 14, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA02891Floorbeam · corrodedFLOORBEAM CORRODED STA 620 FROM BL 0 TO LBL 45. REMOVED, FABBED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 620 FROM BL 0 TO LBL45 ALL IAW FX SR 27-53-034E FIG 1 & 4,FX B727 SRM 51-10-2,BAC5619(H) AND BAC5701.Sep 14, 2005 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA02888Frame · crackedFWD ENTRY DOOR, LWR FRAME IS CRACKED, AT THE LWR FWD CORNER. REPLACED FWD ENTRY DOOR LWR FWD CORNER FRAME IAW SRM 51-30-2, 51-30-5.Sep 14, 2005 · N268FE · Boeing 727233 · Passenger/Crew DoorsSDR 05FDEA02828Shear Tie · corrodedFWD CARGO CORROSION FLOOR SHEAR TIE STA 680 LBL 4 TO RBL 4 WL 148. REPAIRED PER SRM 53-10-4.Sep 9, 2005 · N268FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 05FDEA02827Shear Tie · corrodedFWD CARGO CORROSION (C53-113-01) FLOOR SHEAR TIE STA 640 RBL 4 TO LBL 4 WL 148. REPAIRED PER SRM 53-10-4, MINOR REPAIR.Sep 9, 2005 · N268FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 05FDEA02826Retainer · corrodedCORROSION, RT FWD EMERG EXIT DOOR, PRESSURE SEAL RETAINER AND FASTENERS CORRODED AT LOWER SIDE OF DOOR. REPLACED WITH NEW RETAINER PER FED EX MM 52-21-112-4.Sep 9, 2005 · N268FE · Boeing 727233 · Emergency ExitsSDR 05FDEA02829Shear Tie · corrodedFWD CARGO CORROSION FLOOR SHEAR TIE STA 660 RBL 4 TO LBL 4 WL 148. REPAIRED PER SRM 53-10-4.Sep 9, 2005 · N268FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA02811Web · crackedLOWER CARGO DOOR INNER WEB IS CRACKED 3 INCHES FROM FWD SIDE AFT AND 11 INCHES FROM BOTTOM UP. REPAIRED PER SRM 51-40-2, MINOR REPAIR.Sep 8, 2005 · N268FE · Boeing 727233 · Cargo/Baggage DoorsSDR PCSA0906051Proximity Switch · faultyFLIGHT 713 DURING TAKEOFF ROLL OUT OF MIA CREW REPORTED NUMBER (5) LEADING EDGE SLAT AMBER LIGHT ILLUMINATED ON FLIGHT ENGINEERS PANEL. THE CREW ABORTED THE TAKEOFF & RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE FOUND NUMBER (5) LEADING EDSep 6, 2005 · N994AJ · Boeing 727233 · Trailing Flap Position Indicating SystemSDR 05FDEA02739Channel · damagedWHILE WORKING FED EX EA 7-5330-72293B PT2 FOUND 2 FASTENER HOLES ON EDGE OF "C" CHANNEL BS 620 LBL-36 W/L 292. REPAIRED C-CHANNEL, BS 620, LBL 36 PER FED-EX EA 7-5330-92321.Sep 2, 2005 · N218FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 05FDEA02738Skin · damagedFOUR HOLES BS 620 STR 2L BUCKTAILS BEHIND EXISTING STRUCTURE. REPAIRED HOLES, BS 620, STR 2L PER FED-EX EA 7-5330-92260A.Sep 2, 2005 · N218FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA02728Actuator · malfunctionedLOST SYS A QTY DESCENDING OUT OF 12K FT. RAN APPROPRIATE CHECKLISTS INCLUDING MAN FLAP AND GEAR EXT. NR 7 SPOILER FAILED TO EXT DURING FLAP EXT. REMOVED AND REPLACED NR 7 SLAT ACT IAW M/M 27-81-032-4. REMOVED AND REPLACED CASE DRAIN FILTERS IAW M/M29-11-04Sep 1, 2005 · N285FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 05FDEA02717Tube · chafedHYD SYS A FAILED (W/FLAPS 15) WHILE CONFIGURING TO LAND AT MEM. REPLACED ENGINES NR 1 AND 2 ENGINE DRIVEN HYDRAULIC PUMPS, REF MM29-11-041-2. REPLACED BOTH CASE DRAIN FILTERS. REPLACED SYSTEM "A" HYDRAULIC RETURN FILTER, R/I. REMOVED AND REPLACED SYSTEM A Aug 30, 2005 · N222FE · Boeing 727233 · Hydraulic System, MainSDR 05FDEA02596Frame · damagedWHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND FASTENER HOLES ON EDGE OF FRAME WITH NO EDGE DISTANCE, BS 620 LBL-9 W/L 302 AND 303 2 EA. REPAIRED FRAME BS 620, LBL 9 PER FED-EX EA 7-5330-92323.Aug 23, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA02543Pressure Switch · failedEN ROUTE AT FL 350, IN AND OUT OF POSSIBLE ICING CONDITIONS, WHEN INITIATING WING A/I ON, RECEIVED AIR SYS 3 OFF (LEVEL 1) ANNUNCIATED, WITH NR 3 BLEED (AMBER) AND NR 3 MANF (RED) LIGHTS ILLUMINATED. QRH PROCEDURES FOLLOWED. DIVERTED INTO TO KDEN. RED MANF Aug 18, 2005 · N303FE · Boeing 727233 · Airfoil Anti/De-ice SystemSDR 05FDEA02474Frame · damagedWHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND DOUBLE HOLES IN FRAME AND C-CHANNEL AT 620 RBL 8 W/L 304. (OPEN)Aug 16, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA02473Frame · damagedWHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND FASTENER HOLES ON EDGE OF C-CHANNEL FRAME BS 620 STR 2 RT. REPAIRED PER SRM 53-10-1.Aug 16, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA02472Frame · damagedWHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND DOUBLE HOLE IN FRAME "C' CHANNEL AND SUPPORT AT BS 620 LBL 22 WL 300. REPAIRED C-CHANNEL, BS 620, LBL 22 PER FED-EX EA 7-5330-62327.Aug 16, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA02471Frame · damagedWHILE WORKING FED EX EA 7-5330-72293B PT 2 FOUND DOUBLE HOLE IN FRAME 620 LBL 7 AND LBL 8 W/L 298. FRAME REPLACED PER FED-EX EA 7-5330-92326.Aug 16, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA02381Motor · malfunctionedO/B T/E FLAPS WOULD NOT POSITION WITH FLAP HANDLE. FLT CREW C/W QRH PROCEDURES AND HAVE A C/B PULLED. INSPECTED O/B FLAPS FOR POSSIBLE JAM AND NONE NOTED. WITH HYD ON, THE O/B FLAP CONTROL VALVE IS BYPASSING FLUID. REMOVED AND REPLACED O/B FLAP HYD MOTOR Aug 10, 2005 · N277FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 05FDEA02232Doubler · gougedMAIN CARGO DOOR FORWARD SIDE FRAME GOUGED ON REPAIR DOUBLER MIDWAY UP DOOR. INSTALLED NEW RAPAIR DOUBLER PER FED EX EZA 7-5230-92257Aug 3, 2005 · N218FE · Boeing 727233 · Cargo/Baggage DoorsSDR 05FDEA02164Attach Fitting · corrodedCORROSION (27X5710-02) NR 8 FLAP TRACK FWD ATTACH FTG ON WING IS CORRODED ON I/B FACE. REPAIRED FITTING PER EA 7-5750-92237Aug 1, 2005 · N218FE · Boeing 727233 · Wing, Attach FittingsSDR PCSA0719051Pcu · malfunctionedON TAXI OUT, ACFT ELEVATOR NOSE DOWN STIFF, NOSE UP NORMAL. TAXIED ACFT BACK TO RAMP. VISUAL INSP & TEST OF LT & RT ELEVATOR CABLE SYS & PERFORMED CK OF ELEVATOR CONTROL SYS. OP’S & LEAK CHECK OF ELEVATOR FEEL CONTROL UNIT ACCOMPLISHED, NO DEFECTS NOTED. INSJul 19, 2005 · N994AJ · Boeing 727233 · Elevator Control SystemSDR 05FDEA01965Frame · chafedFUSELAGE UPPER LOBE, FRAME REPAIR IS CHAFED, BS 970, STR 9R. REPAIRED FRAME PER SRM 51-40-3.Jul 15, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA01964Frame · chafedFUSELAGE UPPER LOBE, FRAME IS CHAFED, BS 990, STR 9R. REPAIRED FRAME PER SRM 51-40-3.Jul 15, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA01943Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950B, STR 6L. REMOVED AND REPLACED STR CLIP PER SRM 51-30-2.Jul 14, 2005 · N218FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 05FDEA01942Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950A, STR 7L . REMOVED AND REPLACED STR CLIP PER SRM 51-30-2.Jul 14, 2005 · N218FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 05FDEA01948Bulkhead · corrodedBS 870 BULKHEAD HAS CORROSION ON FWD AND AFT SIDE AT WIRE CONNECTOR ATTACH PLATE, LBL 42. REMOVED CORROSION, FABRICATRED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-1, 51-30-2 AND 53-10-9.Jul 14, 2005 · N218FE · Boeing 727233 · Fuselage Main, BulkheadSDR 05FDEA01947Frame · damaged3 FIGURE 8 HOLES AT BS 460 FRAME VERTICAL FLANGE STR 5R. REPLACED FRAME PER SRM 51-30-2.Jul 14, 2005 · N218FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA01946Web · damagedFIG 8 HOLE AT BS 640 STR 5R FRAME WEB. REPLACED FRAME PER SRM 51-30-2.Jul 14, 2005 · N218FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 05FDEA01928Stringer Clip · crackedFUSELAGE UPPER LOBE, CRACKED STRINGER CLIP, BS 560, STR 7R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-.Jul 13, 2005 · N218FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 05FDEA01927Stringer Clip · crackedFUSELAGE UPPER LOBE, CRACKED STRINGER CLIP, BS 580, STR 7R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2.Jul 13, 2005 · N218FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 05FDEA01926Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950B, STR 8R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2.Jul 13, 2005 · N218FE · Boeing 727233 · Fuselage Main, Attach Fittings
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