Boeing 727-247

Service difficulty reports · 2,669

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '727247'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS97222501Seat Track · corrodedINSPECTION TYPE-S, SEAT TRACK STA 485 TO 490 RBL 25 HAS CORROSION ON FLANGE WL 207. CORROSION OUT OF LIMITS PER SRM 53-10-1. REMOVED AREA OF DAMAGE AND SPLICED IN NEW SECTION OF TRACK PER MM 51-20-151, SRM 51-30-2, 53-10-5, 51-20-10.Mar 19, 1997 · N209UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222500Seat Track · corrodedINSPECTION TYP-SI, SEAT TRACK CORRODED STA 380 TO 440 LBL 45 WL 207. CORROSION OUT OF LIMITS PER SRM 53-10-1. REPLACED TRACK STA 330 TO 440 LBL 45 WITH NEW ITEM PER SRM 53-10-1, 51-30-3, 51-30-2.Mar 19, 1997 · N209UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222499Splice · corrodedINSPECTION TYPE-SI, SEAT TRACK SPLICE STRAPS CORRODED STA 690 RBL 25 AND 45 WL 205. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED REPAIR PARTS AT STA 690 RBL 25 AND RBL 45 PER SRM 53-10-5, 51-30-2, 51-10-2, MM 51-20-151.Mar 19, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222470Hat Channel · corrodedINSPECTION TYPE:SI, CORROSION ON HAT CHANNEL, STA 344 RBL 14-58 WL 207. BLEND CORROSION, BEYOND LIMITS, REMOVED AND REPLACED HAT CHANNEL PER SRM 53-10-1, 51-30-2, AND 51-30-5.Mar 19, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222446Seat Track · corrodedINSPECTION TYPE-SI, SEAT TRACK STA 720B + 10 HAS CORROSION ON FLANGE LBL 25 WL 207. SEAT TRACK FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED AFFECTED SECTION OF SEAT TRACK WITH NEW ITEM PER SRM 53-10-5, 57-10-2.Mar 19, 1997 · N209UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222432Beam · corrodedINSPECTION TYPE-SI, CORROSION ON BEAM STA 440 LBL 29 WL 207 ON TOP CHORD. REMOVED DAMAGED AREA, INSTALLED STANDARD REPAIR SPLICE PER SRM 53-10-1, 53-10-2, 53-10-8 AND MM 51-20-151.Mar 19, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222625Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION ON LOWER CHORD OF FLOORBEAM BS 1130 LBL 10 TO 40 WL 202. REMOVED AND REPLACED LWR CHORD BS 1130 LBL 10 TO 40 WL 202 IAW EWO 97-2120 FILE NR 727-53-1890 UPS.Mar 18, 1997 · N209UP · Boeing 727247 · Fuselage Main, Floor BeamSDR UPS97222542Crease Beam · brokenINSPECTION TYPE-SI, CREASE BEAM BROKEN AT BS 610 AND BS 625 WL 208 RBL 63. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, TREATED PARTS AND INSTALLED PER 727 SRM 51-40-4, 51-10-2, 51-20-4, 51-30-2, MM 51-20-0.Mar 18, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222480Shear Tie · corrodedINSPECTION TYPE:SI, CORROSION ON SHEAR TIE AT STA 950B RBL 12, WL140. BLENDED CORROSION WAS BEYOND LIMITS, CUT OUT DAMAGE, FABRICATED PARTS, INSTALLED REPAIR PER SRM 53-10-4, 51-30-2, 51-10-2, 51-10-6 AND MM 51-20-151.Mar 18, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980605Rib · crackedFOUND ON B2 LETTER CK, .25 INCH CRACK BEYOND PREVIOUS STOP DRILLED CRACK, OUTBD NOSE RIB AT NR 5 SLAT ACTUATOR ROD END. REPAIRED PER MM 57-54-0.Mar 18, 1997 · N295WA · Boeing 727247 · Leading Edge DevicesSDR UPS97222504Torque Box Web · crackedINSPECTION TYPE-SI, CRACK IN WEB AT LIGHTENING HOLE IN TORK BOX BS 1235 RBL 21. CRACK AT BS 1235 RBL 21 WAS STOP DRILLED, WEB PATCH WAS FABRICATED AND INSTALLED PER SRM 51-40-2, 51-20-31, 51-10-2.Mar 17, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222498Seat Track · corrodedINSPECTION TYPE-SI, CORROSION IN HOLE ON SEAT TRACK BS 691 WL 208 RBL 45. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED PORTION OF SEAT TRACK AND INSTALLED NEW IAW SRM 53-10-5, 51-20-21, 51-30-1.Mar 17, 1997 · N209UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222497Skin · gougedINSPECTION TYPE-SI, SEVERAL GOUGES IN SKIN AT LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUTOUT BS 540 RBL 27 WL 155. WHILE WORKING ABOVE ITEM, FOUND CORROSION ON INTERCOSTAL STA 540 RBL 27 WL 155, OUT OF LIMITS PER SRM 53-10-1. REPLACED INTERCOSTAL WITH NEWMar 17, 1997 · N209UP · Boeing 727247 · Fuselage Main, Plate/SkinSDR UPS97222447Intercostal · corrodedINSPECTION TYPE-SI, CORROSION ON INTERCOSTAL BS 623 RBL 26 WL 152 LOWER AFT CORNER OF FWD CARGO DOOR CUTOUT. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. REPLACED INTERCOSTAL WITH NEW PART PER SRM 51-10-2, 51-20-4 MM 51-20-151.Mar 17, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222502Intercostal · corrodedINSPECTION TYPE-SI, CORROSION ON INTERCOSTAL BETWEEN STA 950A + 10 LBL 5 WL 139. CORROSION OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-2, 51-30-5, 51-30-2 AND MM 51-20-151.Mar 15, 1997 · N209UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W970476Indicator · inoperativeOUTBOARD FLAPS IND. 25/25 FLAPS 30 SELECTED. AT APPROXIMATELY 200 FEET, GPWS WARNING FLAPS. PERFORMED GO AROUND I.A.W. DELTA PROCEDURES AND COMPLIED WITH P.O.M. NOTE ALT FLAP MASTER USED. REPLACED OUTBOARD FLAP IND AND RESET. CKS OK PER MM CHAPT. 27.Mar 13, 1997 · N2821W · Boeing 727247 · Trailing Flap Position Indicating SystemSDR DL72W970481Frame · crackedFOUND ON A-1 LETTER CHECK, .3750 INCH VISIBLE CRACK IN MLG UPLOCK SUPPORT FRAME OTBD FLANGE AT STA 910. REPAIRED PER MM 53-11-0.Mar 11, 1997 · N296WA · Boeing 727247 · Fuselage Main, FrameSDR DL72W970464Angle · crackedFOUND DURING A-1 LETTER CHECK - 1 INCH VISIBLE CRACK NR 1 SLAT ACTUATOR INBOARD ATTACH BRACKET. REPAIRED PER M/M 57-20-21.Mar 11, 1997 · N296WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W970436Hyd Module · crackedSYS-A HYD QTY LEAKED BELOW 2.5 GALS COMPLETED POM PROCEDURES LEAK STOPPED WITH PRESSURE OFF. FOUND A-SYS MODULE LEAKING. BORROWED PART FROM FEDX (S/N 260SA), INSTALLED. PERFORMED OPERATIONAL CK OUT, ALL NML NO LEAKS.Mar 8, 1997 · N2807W · Boeing 727247 · Hydraulic System, MainSDR UPS97222280Shear Tie · corrodedINSPECTION TYPE-C, CORROSION ON SHEAR TIE AFT SIDE OF FRAME BS 990 RBL 10 WL 137. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-02, 51-40-03, CORRODED PART OUT OF LIMITS PER SRM 53-10-1.Mar 7, 1997 · N208UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222281Nose Chord · corrodedINSPECTION TYPE-C, CORROSION ON UPPER NOSE CHORD BS 294.5 TO 297 LBL 14 WL 175 ON LOWER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. INSTALLED NEW CHORD IAW SRM 51-10-1, 51-30-2.Mar 3, 1997 · N208UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS97222279Skin · delaminationINSPECTION TYPE-C, NR 10 SPOILER HAS DELAMINATION AT THE UPPER SURFACE LEFT HAND CORNER. REMOVED DAMAGE, REPAIRED IAW SRM 51-40-6.Mar 2, 1997 · N208UP · Boeing 727247 · SpoilersSDR UPS97222278Skin Patch · disbondedINSPECTION TYPE-C, L/W INBOARD FOREFLAP HAS A LARGE PREVIOUS REPAIR DISBONDED UPPER SURFACE MID SPAN. REMOVED PREVIOUS REPAIR, INSTALLED A NEW REPAIR IAW SRM 51-40-6.Mar 2, 1997 · N208UP · Boeing 727247 · Trailing Edge FlapsSDR DL72E970362Battery Pack · dischargedAFT CABIN EMERGENCY LIGHTS OUT. REPLACED BATTERY PACK M983.Feb 26, 1997 · N831WA · Boeing 727247 · Emergency LightingSDR DL72W970354Fitting · crackedFOUND A 1 INCH CRACK IN RT ELEVATOR HINGE SUPPORT CASTING 4TH HINGE FROM O/B END. REPAIRED PER M/M 55-10-31.Feb 25, 1997 · N2817W · Boeing 727247 · Horizontal Stabilizer StructureSDR UPS97222069Stringer · corrodedINSPECTION TYPE-C, WHILE WORKING FUSELAGE 36 FOUND CORRODED STRINGER 26R BS 1146 TO 1183 FOUND STRINGER TO BE OUT OF LIMITS PER SRM 53-10-03. REPAIRED STRINGER PER SRM 51-10-1, 51-10-2, 51-30-2, 53-10-3.Feb 15, 1997 · N210UP · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W970276Hydraulic Pump · inoperativeNR 1 ENGINE HYDRAULIC PUMP CHANGED FOR A SYSTEM PRESSURE LOSS.Feb 13, 1997 · N297WA · Boeing 727247 · Hydraulic Pump (Electric/Engine), MainSDR DL72W970268Power Supply · inoperativeON L/O CK, FOUND RT OVERWING EXIT SIGNS WOULD NOT ILLUMINATE WITH EMER LTS ON. REPLACED POWER SUPPLY AND BATTERY, OPS CKS OK.Feb 12, 1997 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W970265Power Supply · inoperativeON L/O CK, FOUND RT OVERWING EXIT SIGNS WOULD NOT ILLUMINATE WITH EMERGENCY LIGHTS ON. REPLACED POWER SUPPLY AND BATT, OPN CKS OK.Feb 12, 1997 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W970263Actuator · failedLOST ALL HYD SYS A-PRESS AND FLUID 90 MILES FROM AIRPORT. USED ABNORMAL CHECKLIST. REPLACED RUPTURED NUMBER 3 SLAT ACTUATOR.Feb 12, 1997 · N297WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W970296Start Valve · failedDURING CLIMBOUT, NR 1 ENG START VLV LIGHT ILLUMINATED. REPLACED START VLV AND PRESS SW.Feb 10, 1997 · N2812W · Boeing 727247 · Engine Start Valves/ControlsSDR UPS97222070Frame · corrodedINSPECTION TYPE-C, CORROSION ON FRAME OUT OF LIMITS STA 950B LBL 9 WL 138. FABRICATED AND INSTALLED NEW ANGLE AND DOUBLERS ALL IAW SRM 53-10-2, 51-30-3.Feb 7, 1997 · N210UP · Boeing 727247 · Fuselage Main, FrameSDR 97FDEA00093Sensor · inoperativeAFTER GEAR RETRACTION ON TAKEOFF, THE RED RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR UNSAFE AND/OR DOORS LIGHT. GEAR HANDLE UP, CHECKLIST WAS ACCOMPLISHED DOWN TO ITEM 3B THE FLIGHT WAS CONTINUED AND MONITORED AS PER CHECKLIST. REMOVED AND REPLAFeb 7, 1997 · N237FE · Boeing 727247 · Landing Gear Position and WarningSDR 97FDEA00090Uplock Sensor · out of adjustON TAKEOFF, THE RIGHT GEAR RED LIGHT ILLUMINATED. UNSAFE DOOR LIGHT CHECK LIST WAS READ TO STEP 3B. LIGHT WENT OUT IN 20 MINUTES. LIGHT CAME ON PASSING 11000 FEET AT 300 KNOTS. ADJUSTED GAP ON UPLOCK SENSOR AND TARGET. OPERATIONAL CHECK GOOD ON UPLOCK SENFeb 6, 1997 · N237FE · Boeing 727247 · Landing Gear Position and WarningSDR UPS97221923Hinge Lug · crackedNR 1 KREUGER FLAP HAS CRACK ON CENTER HINGE LUG AT BOTTOM BOLT HOLE. REPLACED NR 1 KREUGER FLAP IAW MM 27-81-01. SYS OP/C NORMAL. LANDING LIGHT OP/C NORMAL.Feb 1, 1997 · N210UP · Boeing 727247 · Leading Edge DevicesSDR UPS97221872E1 Rack · water contamON FINAL APPROACH, FLAPS WERE SELECTED TO 2 DEGREES. ALL POWER TO AIRCRAFT WAS LOST EXCEPT CAPTAIN'S INSTRUMENTS. ALL LIGHTS DIMMED AND NO INDICATION ON ENGINEER'S PANEL (PANEL WAS DARK) AFTER A PACK WAS DOWNLOADED. POWER CAME BACK ON. NR 1 AND NR 2 BUS. FJan 28, 1997 · N211UP · Boeing 727247 · Electrical Power SystemSDR DL72W970216Skin · corrosionCORROSION WAS FOUND ON THE FUSELAGE LOWER SKIN BETWEEN AT 681 AND 720 JUST I/B OF STR 26R IN THE VICINITY OF AN EXISTING REPAIR. THE EXISTING DOUBLER WAS REMOVED AND A SINGLE REPAIR COVERED BOTH AREAS. THIS REPAIR IS APPROVED BY FAA/DER FORM 8110-3, DER DESIJan 27, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E970215Stiffener · corrosionCORROSION WAS DISCOVERED AT THE LOWER END OF LBL 17.8 VERTICAL STIFFENER, JUST BELOW THE SUPPORT ROD END AT STA 1183. CORROSION IS ON THE O/B FACE OF THE VERTICAL WEB WHICH RUNS FWD-AFT. THIS DAMAGE HAS BEEN REPAIRED IN ACCORDANCE WITH S/B 727-53-0202.Jan 18, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E970087Web · crackedLT TORQUE BOX VERTICAL WEB LIGHTENING HOLE CRACKED 2 PLACES AT STA 1235, MARKED. REPAIRED PER M/M 53-11-0 PG 828.Jan 17, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E970085Web · crackedLT TORQUE BOX VERTICAL WEB LIGHTENING HOLE CRACKED 2 PLACES AT STA 1235. INSTALLED DOUBLER PER MM 53-11-0 PG 828.Jan 17, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous StructureSDR 97FDEA00051Fire Light · illuminatedON CLIMBOUT, THE NR 2 FIRE SYSTEM SOUNDED AND THE WARNING LIGHTS ON THE GLARE SHIELD ILLUMINATED FOR ABOUT 3 TO 4 SECONDS AND THEN WENT OUT. THE WARNING SOUNDED AGAIN ABOUT 30 SECONDS LATER FOR 3 TO 4 SECONDS AND THEN WENT AWAY. ALL ENGINE PARAMETERS WERE NOJan 17, 1997 · N236FE · Boeing 727247 · Fire DetectionSDR DL72W970190Skin · gougedDURING THE INSTALLATION OF THE UPPER HINGE REPAIR/MODIFICATION PER 727-53-0198, A GOUGE WAS FOUND IN THE LOWER FUSELAGE SKIN JUST AFT OF THE REPAIR AREA. DAMAGE REMOVAL RESULTED IN A 1 INCH BY 2 INCH CUT-OUT IN THE SKIN. DUE TO THE CLOSE PROXIMITY OF THIS DAJan 16, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W970102Skin · crackedAT MIDVISIT, THE SKIN AT GROUND PNEUMATIC DUCT ACCESS DOOR WAS FOUND CRACKED AT THE AFT I/B CUTOUT CORNER. A DOUBLER WAS FABRICATED AND DRILLED AND INSTALLED PER MM 53-30-0 FIG 802.Jan 16, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W970191Skin · crackedTWO CRACKS IN THE SKIN AND DOOR SURROUND STRUCTURE WERE FOUND IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE FIRST CRACK MEASURES APPROXIMATELY 2.25 INCHES AND PENETRATES THE EXTERNAL SKIN AND BONDED DOUBLER. THE SECOND CRACK MEASURES APPROXIMATELY 2.25 Jan 15, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W970180Angle · corrosionCORROSION ON MOUNT ANGLES AROUND PERIPHERY OF LOWER FUSELAGE FAIRING OPENING AFT OF LOWER ROTATING BEACON. BEGAN REMOVING T-ANGLES FROM STA 820-920. FABRICATED NEW REPLACEMENT PARTS FOR RT BEAM PER SRM 53-30-1. COMPLETED INST OF RT ANGLE. FABRICATED LT BEJan 14, 1997 · N2815W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W970130Bulkhead · crackedAT MIDVISIT THE BULKHEAD WEB WAS FOUND CRACKED AT BOTH LOWER O/B CORNERS AT FS 1303. THIS WAS REPAIRED PER SRM 53-10-4.Jan 14, 1997 · N2815W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W970115Door Frame · crackedFOUND R-2 DOOR FRAME CRACKED AT UPPER HINGE CUTOUT. FABRICATED DOUBLER PER SRM 52-40-2 FIG 4. ROUTED OUT DAMAGE PER SRM 52-40-2 FIG 4, INSTALLED DOUBLER PER SRM 52-40-2 FIG 4.Jan 14, 1997 · N2815W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W970048Battery · dischargedFWD EMERGENCY FLASHLIGHT WON,T BLINK. REPLACED FLASHLIGHT BATTERY AND BULB, OPERATIONAL TEST NML.Jan 10, 1997 · N2820W · Boeing 727247 · Emergency LightingSDR DL72W970034Stiffener · crackedL/E VERTICAL SPAR STIFFENER CRACKED AT NR 3 SLAT O/B TRACK I/B STIFFENER. REPLACED STIFFENER PER MM 57-20-21.Jan 8, 1997 · N2815W · Boeing 727247 · Leading Edge DevicesSDR DL72E970192Tie Bolt · shearedTHE INBOARD TENSION TIE BOLT AT THE RT S-3A WAS FOUND SHEARED. THIS PROBLEM IS THE SUBJECT OF BACO S/B 727-53-0178, REV 2. THE BOLT WAS REPLACED AND THE TENSION TIE FITTING WAS INSPECTED IN ACCORDANCE WITH THE SERVICE BULLETIN.Jan 8, 1997 · N282WA · Boeing 727247 · Fuselage Miscellaneous Structure
Back to Boeing 727-247