Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR AALA20011596Wire · brokenRDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 16 THROUGH 18 INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 5, 2001 · N731AA · Boeing 727227 · Emergency LightingSDR AALA20011557Connector · damagedDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING FROM AFT TO FORWARD OF CABIN DIMMING. REPLACED DAMAGED CONNECTOR AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 3, 2001 · N730AA · Boeing 727227 · Light System WiringSDR CA010808061Fire Loop · corroded(CAN) ON FINAL APPROACH INTO YMX PILOTS RECIEVED WHEEL WELL FIRE INDICATION, WHEEL WELL LIGHT ON WITH THE FIRE BELL.PILOTS CARRIED OUT EMERGENCY CHECKLIST DECLARED AN EMERGENCY. PILOTS LANDED WITH NO FURTHER PROBLEMS. UPON INSPECTION IT WAS NOTED THAT THE COAug 3, 2001 · Boeing 727227 · Fire DetectionSDR XNA01016Engine · overtempNR 2 OIL TEMP GAUGE INDICATED 130 DEGREES. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AS PER CHECK LIST.Aug 1, 2001 · N793A · Boeing 727227 · Engine (Turbine/Turboprop)SDR AALA20011584Skin · corrodedTUL - FOUND CORROSION AROUND FASTENER HEAD LOWER SKIN OF WING CENTER SECTION LBL 24 STRINGER 6. REPAIRED PER ESO 11697 DATED 7/31/2001 EXTERNAL DOUBLER. (M)Jul 31, 2001 · N716AA · Boeing 727227 · Wing, Plate/SkinSDR AALA20011583Skin · corrodedTUL - FOUND CORROSION ON LOWER WING SKIN IN AREA OF PREVIOUS REPAIR ABOVE LEFT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697 DATED 7/31/2001 EXTERNAL DOUBLER. (M)Jul 31, 2001 · N716AA · Boeing 727227 · Wing, Plate/SkinSDR AALA20011587Skin · corrodedTUL - FOUND FUSELAGE SKIN BULGED STATION 992 STRINGER 29R. REMOVED CORRODED AREA OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M)Jul 31, 2001 · N716AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA20011586Stringer · corrodedTUL - FOUND STRINGER 29R CORRODED ON LOWER FLANGE AT STATION 998. INSTALLED NEW STRINGER SECTION WITH SPLICE PER SRM 53-10-3. (M)Jul 31, 2001 · N716AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011585Skin · corrodedTUL - FOUND LIGHT CORROSION AROUND FLAPPER DRAIN BETWEEN 28R AND BLO STATION 685. INSTALLED DOUBLER PER SRM 53-30-3 050 7075 T-6 9 INCH BY 9 INCH FOUR ROWS EACH SIDE .1875 RIVETS. (M)Jul 31, 2001 · N716AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011577Skin · corrodedTUL - FOUND CORROSION ON INTERIOR OF SKIN BETWEEN STATION 1148 AND STATION 1166 BETWEEN STRINGER 22L AND 23L. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED JULY 27, 2001. (M)Jul 31, 2001 · N720AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011579Web · crackedTUL - FOUND LEFT PRESSURE WALL IS CRACKED JUST BELOW DOOR CABLE QUAD. INSTALLED DOUBLER PER ESO 11697 7/30/01. (M)Jul 30, 2001 · N720AA · Boeing 727227 · Standard Practices/StructuresSDR AALA20011578Angle · corrodedTUL - FOUND LEADING EDGE WING SKIN BULGED AT UPPER SPAR ATTACH SCREWS 8 INCH - 9 INCH OUTBOARD OF FUSELAGE. REMOVED CORROSION TREATED AND PRIMED AREA AND INSTALLED A STRAP AND ANGLES WITH DOUBLER REPAIR PER ESO 11697 DATED 7/27/2001. (M)Jul 29, 2001 · N720AA · Boeing 727227 · Wing Miscellaneous StructureSDR AALA20011607Door Frame · crackedTUL - FOUND LEFT AFT GALLEY DOOR FORWARD JAMB CRACKED AT TOP FORWARD SIDE. STOP DRILLED CRACK INSTALLED DOUBLER PER ESO 11697 DATED 7-26-2001. (M)Jul 27, 2001 · N716AA · Boeing 727227 · Fuselage Main, StructureSDR AALA20011576Skin · corrodedTUL - FOUND SKIN BULGING AFT OF 480 BUTT SPLICE STRINGER 28 LEFT, 14 INCHES BY 2 INCHES. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR AND FILLER PER SRM 53-30-03 FIG 3A. (M)Jul 27, 2001 · N720AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA20011606Stiffener · corrodedTUL - FOUND STIFFENER CORRODED ON 870 BULKHEAD 1ST STIFFENER OUTBOARD OF KEEL BEAM, ON OUTBOARD SIDE APPROX MIDDLE OF STIFFENER. DAMAGE, REMOVED HFEC INDICATED NO CRACK AROUND ELONGATED BLENDED HOLE, DOUBLER INSTALLED PER ESO11697 DATED 7-24-01. (M)Jul 26, 2001 · N716AA · Boeing 727227 · Standard Practices/StructuresSDR AALA20011496Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTING FORWARD SECTION INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jul 25, 2001 · N717AA · Boeing 727227 · Emergency LightingSDR AALA20011582Light · inoperativeTUL - FOUND LIGHT WOULD NOT OPERATE IN ARM POSITION. REPLACED LIGHT ASSEMBLY. OPS CHECKED GOOD. (M)Jul 24, 2001 · N716AA · Boeing 727227 · Emergency LightingSDR AALA20011605Spar Cap · corrodedTUL - FOUND LEFT HORIZONTAL STAB, REAR SPAR CAP EXTENSION, ON AFT END, HAD CORROSION ABOVE NR 1 ELEVATOR HINGE. INSTALLED DOUBLER AND FILLER REPAIR PER ESO 11697 DATED 7-23-2001. (M)Jul 24, 2001 · N716AA · Boeing 727227 · Horizontal Stabilizer, Spar/RibSDR CA010727016Tire · failed(CAN) THE NR 1 TIRE THREAS SEPARATED FROM THE CARCASS DURING T/O ROTATION. DAMAGE ON EXTERIOR OF THE WING DOOR. THE NR 2 TIRE FAILED ON TAXI INTO RAMP IN YYC.Jul 18, 2001 · Boeing 727227 · TireSDR AALA20011400Light · defectiveTUL - FOUND FLOOR EMERGENCY ESCAPE PATH LIGHTING STRIP WEAK, DIM, FROM FORWARD GALLEY TO AFT GALLEY. INSTALLED NEW PATH LIGHT AND CLEAR LENS. OPS CHECK OK. (M)Jul 11, 2001 · N726AA · Boeing 727227 · Emergency LightingSDR 01FDEA00534Proximity Switch · faultyMAIN CARGO DOOR LIGHT ILLUM. PERFORMED QUICK REF HDBK PROC. DIVERT TO MSP. *S/D* REMOVED AND REPLACED MCD CTR PROX SW 29038 PER MM 52-34-009-5. AC OK FOR SERVICE.Jul 11, 2001 · N486FE · Boeing 727227 · Door Warning SystemSDR AALA20011409Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE BS 720A AT STRINGER 28. REMOVED CORROSION AND REMOVED DAMAGED AREA, AND REPAIRED PER SRM 53-10-04. (M)Jul 9, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011411Trunnion · corrodedTUL - FOUND CORROSION IN NOSE GEAR TRUNNION FITTINGS. CORROSION REMOVED, NOSE GEAR TRUNNION FITTINGS WERE REBORED AND REBUSHED PER ESO 11697 DATED 7/6/2001. (M)Jul 9, 2001 · N731AA · Boeing 727227 · Nose/Tail Landing Gear Attach SectionSDR XNA01012FIndicator · faultyON TAXI OUT FLAPS INDICATED SPLIT AND ASYMMETRICAL SETTING. REMOVED AND REPLACED I/B FLAP POSITION INDICATOR. OPS CHECKS GOOD IAW 27-52-0 B727 MM.Jul 8, 2001 · N793A · Boeing 727227 · Trailing Flap Position Indicating SystemSDR AALA20011410Beam · corrodedTUL - FOUND LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED SS136 TO SS142. REMOVED CORROSION, INSTALLED DOUBLER REPAIR PER ESO 11697 DATED 7-6-01. (M)Jul 6, 2001 · N731AA · Boeing 727227 · Horizontal Stabilizer StructureSDR AALA20011402Skin · bulgedTUL - FOUND SKIN BULGING AT RIVETS, RIVETS DISHED ON SKIN LAP 24R STATION 343 TO 360. REPAIRED AREA PER SRM 53-30-4 FIG 16. (M)Jul 6, 2001 · N726AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA20011403Skin · corrodedTUL - FOUND SKIN BULGING IN AREA PREVIOUSLY WORKED, SKATE ANGLE (APPEARS TO BE RE-CORRODING) JUST ABOVE RIGHT NOSE GEAR STRUT DOOR .294.5 TO 335. SKIN BULGING AROUND REPAIR AREA FASTENERS, SIX INCHES ABOVE SKATE ANGLE STATION 295-333. REPAIRED AREA PER ESO 1Jul 6, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011401Frame · dentedTUL - FOUND BELT FRAME DENTED AT STATION 1050 OVER STRINGER 26L. CUT OUT DAMAGE AND INSTALLED BELT FRAME REPAIR PER 53-10-4 PAGE 1. (M)Jul 6, 2001 · N726AA · Boeing 727227 · Fuselage Main, FrameSDR AALA20011412StringerTUL - FOUND RIVETS HEADS POPPED AND SKIN BULGED AT STRINGER 21R JUST AFT OF STRINGER 440. REMOVED CORRODED SECTION OF STRINGER 21R AND INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M)Jul 5, 2001 · N731AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011404Stringer · corrodedTUL - FOUND CORROSION IN BOTTOM OF STRINGER 26R. REPAIRED STRINGER PER SRM SB 53-10-3 AND BOTTOM WITH BOLTS, NUTS AND WASHERS THRU STRINGER CLIP AND STRINGER SIDES. (M)Jul 5, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011405Beltframe · dentedTUL - FOUND BELT FRAME DENTED STATION 1050 AT STRINGER 25R. INSTALLED BELT FRAME REPAIR PER SRM 51-40-3 PAGE 1. (M)Jul 5, 2001 · N726AA · Boeing 727227 · Fuselage Main, FrameSDR AALA20011406Skin · crackedTUL - FOUND FUSELAGE SKIN CRACKED AT STATION 235 STRINGER 22L. REPAIRED CRACK PER SRM 53-30-3 FIG 3 SHEET 4, CLOSE TO EXISTING REPAIR DOUBLER. INCORPORATED ONE LARGE DOUBLER 16 INCHES BY 8 INCHES TO COVER BOTH AREAS. (M)Jul 4, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011407Frame · crackedTUL - FOUND BELT FRAME CRACKED STATION 312 BETWEEN STRINGER 13, 14 RIGHT SIDE FORWARD LAVATORY. REMOVED DAMAGED SECTION. INSTALLED DOUBLER REPAIR PER RM 53-10-4. (M)Jul 4, 2001 · N726AA · Boeing 727227 · Fuselage Main, FrameSDR AALA20011408Stringer · corrodedTUL - FOUND CORROSION ON STRINGER 23R STATION 720E. REPLACED STRINGER SECTION 720D PLUS 10 TO 720E PLUS 10 SPLICED EPR SRM 53-10-3 FIG 1. (M)Jul 3, 2001 · N726AA · Boeing 727227 · Fuselage Structure (General)SDR XNA01012EControl Panel · contaminatedDURING CLIMB AFTER DEPARTURE, DEVELOPED ASYMMETRICAL INBOARD FLAPS. FOUND EXCESSIVE WATER CONTENT IN INBOARD AND OUTBOARD TRAILING EDGE FLAP POSITION TRANSMITTER C/P. CLEANED AND RESECURED TRANSMITTER C/P'S. REACTIVATED FLAPS AFTER CREW LOCK OUT. SYSTEM OPJul 3, 2001 · N793A · Boeing 727227 · Trailing Flap Position Indicating SystemSDR AALA20011338Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jul 2, 2001 · N718AA · Boeing 727227 · Emergency LightingSDR AALA20011329Wire · brokenDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT JUMPER WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jun 30, 2001 · N723AA · Boeing 727227 · Light System WiringSDR AALA20011328Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT SEAT 8 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jun 30, 2001 · N723AA · Boeing 727227 · Emergency LightingSDR AALA20011399Web · crackedTUL - FOUND RIGHT NOSE GEAR PRESSURE DECK HAS VISUAL INDICATION OF CRACK AT RIVET ABOVE PANEL AT STATION 203. INSTALLED DOUBLER PER SRM 51-40-2 USING .063 2024 T-3 WITH .1875 INCH MS20470D RIVETS AND SIX .1875 INCH HI-LOCKS. (M)Jun 30, 2001 · N726AA · Boeing 727227 · Standard Practices/StructuresSDR XNA01012DStart Valve · failedENGINE NR 3 STARTER SW STARTER VALVE FAILED TO OPEN. TESTER IN MANUAL. VALVE NR 3 ENGINE DEFERRED AS PER MEL 80-3. TRANSFERRED TO DMI 1373.Jun 29, 2001 · N793A · Boeing 727227 · Engine Start Valves/ControlsSDR AALA20011300Stringer · corrodedTUL - FOUND STRINGER 28R IS CORRODED ON OUTBOARD SIDE. REMOVED CORRODED STRINGER AT STATION 950C PLUS 9,5 INCH AND 950 PLUS 8 INCHES. INSTALLED STRINGER FILLERS SPLICE ANGLES PER ESO 11697 DATED 6-22-2001. (M)Jun 24, 2001 · N725AA · Boeing 727227 · Standard Practices/StructuresSDR AALA20011313Stiffener · corrodedTUL - FOUND VERTICAL STIFFENER CORRODED. REMOVED AND REPLACED STIFFENER 51-10-00. (M)Jun 21, 2001 · N725AA · Boeing 727227 · Standard Practices/StructuresSDR AALA20011299Frame · crackedTUL - FOUND BELT FRAME CRACKED STATION 1110, RBL 18 TOP OF FLANGE. REPAIRED BELT FRAME BY CUTTING OUT CRACKED AREA AND INSTALLING REPAIR TO BELT FRAME PER SRM 51-40-3. (M)Jun 21, 2001 · N725AA · Boeing 727227 · Fuselage Main, FrameSDR AALA20011298Stringer · corrodedTUL - FOUND STRINGER 27R CORRODED AT STATION 1130 INBOARD SIDE. REMOVED DAMAGED STRINGER AND INSTALLED NEW STRINGER SECTION AND SPLICE PER SRM 53-10-3. (M)Jun 21, 2001 · N725AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011297Shear Tie · corrodedFOUND FORWARD SIDE OF STATION 520 SHEAR TIE HAS LIGHT CORROSION BETWEEN STRINGER 28 RL. CUT AND REMOVED CORRODED AND CRACKED FLANGE OF SHEAR TIE. FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-10-4 FIG 5. (M)Jun 21, 2001 · N725AA · Boeing 727227 · Fuselage Internal Mounting StructureSDR 01FDEA00477Fuel Cap · faulty01-204 AFT T/O #3 FUEL TANK GAUGE IND LOSS OF FUEL FROM THAT TANK. #3 BOOST PUMPS SHUTOFF & CROSSFEED #3 ENG FROM #1 FUEL TANK. INSTALL NEW FUEL CAP IN ACCORD WITH B727 MM 28-11-031-4. OK TO CONTINUE.Jun 21, 2001 · N496FE · Boeing 727227 · Fuel Dump SystemSDR AALA20011296Shear Tie · corrodedTUL - FOUND SHEAR TIE STATION 720C STRINGER 28 RIGHT CORRODED. REMOVED AND REPLACED SHEAR TIE 51-01 SRM. (M)Jun 20, 2001 · N725AA · Boeing 727227 · Fuselage Internal Mounting StructureSDR AALA20011294Bulkhead · crackedTUL - FOUND CRACK IN WEB BELOW APU LOAD CONTROL VALVE, STATION 870 BULKHEAD 4 INCHES LONG. CRACK IN FS 870 BULKHEAD FORWARD SIDE AT APU CONTROL VALVE BOTTOM OUTBOARD SIDE OF CUTOUT. REPAIRED PER SRM 53-10-2 WITH DOUBLER. (M)Jun 20, 2001 · N725AA · Boeing 727227 · Fuselage Main, StructureSDR AALA20011292Skin · crackedTUL - FOUND SKIN CRACKED AT RIVIT HOLE STATION 328 JUST BELOW STRINGER 206. ALSO, FOUND SKIN CRACKED AT TWO RIVITS STATION 328 JUST BELOW STRINGER 21L. CUT OUT DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M)Jun 20, 2001 · N725AA · Boeing 727227 · Fuselage Structure (General)SDR AALA20011295Light · inoperativeTUL - FOUND AFT SERVICE AND GALLEY DOORS AFT LIGHT ASSEMBLY FOR EACH HAS LAMP OUT IN LIGHT ASSEMBLIES FOR EMERGENCY EXIT. INSTALLED NEW LAMP ASSEMBLY AT AFT SIDE EACH DOOR. OPS CHECKED OK. (M)Jun 19, 2001 · N725AA · Boeing 727227 · Emergency Lighting
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