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 DL72W953368Skin · damagedDURING HMV, FOUND TEMP REPAIR INSTALLED AT FS 1223 RBL 12. REPAIRED PER MM 53-30-0 PAGE 804.Jul 23, 1995 · N2812W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W953367Skin · damagedDURING HMV, FOUND TEMP REPAIRED INSTALLED RIGHT SIDE AFT AND ABOVE PANEL 9516. REPAIRED PER MM 53-30-0 PAGE 801 AND 802.Jul 23, 1995 · N2812W · Boeing 727247 · Nacelle/Pylon, Plate/SkinSDR DL72W953365Support Ring · wornDURING HMV, FOUND NR 2 ENG COWL SUPPORT RING WORN. REPAIRED PER M/M 53-11-0 PAGE 801.Jul 23, 1995 · N2812W · Boeing 727247 · Engine Cowling SystemSDR DL72W953364Web · crackedDURING HMV, FOUND WEB CRACKED AT STA 1278 IN 48 SECTION, LOWER INSP HOLE. REPAIRED PER MM53-11-0 PAGE 832.Jul 23, 1995 · N2812W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W953283Skin · lightning strikeLT ELEVATOR, LIGHTNING DAMAGE L/E TO T/E OB OF TAB. REPAIRED PER SRM 55-20-3 FIG 4, FOUND AT HMV.Jul 23, 1995 · N2812W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W953264Web · crackedVERTICAL WEB INSIDE THE VERTICAL STAB CRACKED AT BASE OF RIB NR 1 AT LT AND RT LOWER CORNERS. REPAIRED PER SRM 53-10-4 FIG 17.Jul 23, 1995 · N2812W · Boeing 727247 · Vertical StabilizerSDR DL72W953262Frame · puncturedFRAME PUNCTURED AT FS 1050 TOP FLANGE ABOVE STR. 27R AND 27L. REPAIRED PER SRM 53-10-4 FIG 27.Jul 23, 1995 · N2812W · Boeing 727247 · Fuselage Main, FrameSDR DL72W953215Skin · gougedRT ELEVATOR GOUGED, .52 BY .1250 BY .040 ON LWR L/E, 2.5 FT I/B OF OB HINGE. REPAIRED PER SRM 55-20-3 FIG 4, FOUND AT HMV.Jul 23, 1995 · N2812W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W953214Te Skin · damagedRT ELEVATOR LIGHTNING DAMAGE ON O/B CORNER T/E. REPAIRED PER MM 55-20-0 PG 801, FOUND AT HMV.Jul 23, 1995 · N2812W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W953266Bracket · crackedNR 1 LE FLAP ACTUATOR MOUNT BRACKET CRACKED AT UPPER AND LOWER CORNERS. REPAIRED BRACKET PER MM 57-20-21 FIG 807.Jul 22, 1995 · N2812W · Boeing 727247 · Leading Edge DevicesSDR DL72W953265Bracket · crackedNR 2 LE FLAP ACTUATOR AFT ATTACH BRACKETS ARE CRACKED ON ALL 4 CORNERS. REPAIRED PER MM 57-20-21 FIG 807.Jul 22, 1995 · N2812W · Boeing 727247 · Leading Edge DevicesSDR DL72W953139Gusset · crackedDURING LETTER CHECK INSPECTION, THE RT TORQUE BOX BEAM GUSSET AT FS 1273 WAS FOUND CRACKED. IN ACCORDANCE WITH B727 S/B 53-0129, REV. 4, THE DAMAGED GUSSET WAS REPLACED.Jul 21, 1995 · N296WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W953131Eel Battery Pack · dischargedEMERG LIGHT, F/C BULLNOSE INOP. REPLACED BATTERY AND RACK, OPERATION NORMAL.Jul 20, 1995 · N2819W · Boeing 727247 · Emergency LightingSDR DL72W953129Doublers · crackedFOUND DURING E-2 LETTER CHECK, NR 3 L/E SLAT ACT ROD END I/B AND O/B SUPPORT RIB DOUBLERS CRACKED. REPLACED DOUBLERS PER M/M 57-54-0 PG 803 TO 805.Jul 20, 1995 · N296WA · Boeing 727247 · Leading Edge DevicesSDR DL72W953128Angle · crackedNR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT I/B STOP PAD. ITEM FOUND DURING E-2 LETTER CHECK. REPAIRED PER MM 57-54-0 PG 807.Jul 20, 1995 · N296WA · Boeing 727247 · Leading Edge DevicesSDR DL72W953127Stringer · crackedFOUND DURING E-2 LETTER CHECK, 1 INCH CRACK IN VERT STAB STRINGER 8 RT AT THIRD BULKHEAD ABOVE CRAWLWAY OPENING FIN STA 133.8. REPAIRED PER MM 55-30-0 PG 803.Jul 20, 1995 · N296WA · Boeing 727247 · Vertical StabilizerSDR DL72E953121Panel · damagedUPON ARRIVAL PDX, FOUND ON RIGHT HORZ STAB LOWER SURFACE A CLOSURE PANEL FOR AN ELEV BALANCE PANEL BAY. PANEL 9216 THE FWD THIRD OF PANEL HAD SEPARATED FROM THE ACFT AND EMBEDDED ITSELF INTO THE TAIL CONE. ALSO, FOUND LOWER SKIN DAMAGED ON RIGHT ELEVATOR. Jul 20, 1995 · N831WA · Boeing 727247 · Horizontal Stabilizer, Plate/SkinSDR USAA950763Window · crackedLGA - FLT 0599 - THE CAPTAINS SLIDING WINDOW CRACKED. CAPTAIN TURNED OFF THE WINDSHIELD HEAT AND RETURNED TO LGA. MAINTENANCE REPLACED THE CAPTAINS SLIDING WINDOW. OPERATIONS CHECKED GOOD. (M)Jul 19, 1995 · N749US · Boeing 727247 · Flight Compartment WindowsSDR DL72W953110Angle · crackedFOUND DURING D-2 LETTER CHECK - ANGLE CRACKED UNDER NR 7 SLAT ANTI-ICE DUCT LOWER AFT END OF SLAT. REPAIRED PER M/M 57-54-0, FIG 805A.Jul 18, 1995 · N2820W · Boeing 727247 · Leading Edge DevicesSDR DL72W953109Skin · crackedFOUND DURING D-2 LETTER CHECK - .75 INCH CRACK IN VERT STAB SKIN RT SIDE JUST AFT OF NR 2 ENG NOSE COWL AT PANEL 9516 . REPAIRED PER M/M 54-30-0, PG 801-802.Jul 18, 1995 · N2820W · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72E953336Skin · dentedDUE TO GROUND DAMAGE, THE RIGHT SIDE OF THE FUSELAGE SUSTAINED DAMAGE. STRINGER 21R WAS SEVERED, THE SKIN DAMAGE WAS CUTOUT BETWEEN FS 660 TO FS 680 TO THE DIMENSIONS 22.5 FORE-AFT BY 20 UP AND DOWN. THE DAMAGED SECTION OF 21R HAS BEEN REMOVED FROM FS 650 TOJul 18, 1995 · N283WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E953087Actuator · faultyON CLIMB AFTER GEAR RETRACTION, NR 1 L/E KRUGER FLAP DID NOT RETRACT. FLIGHT RETURNED TO DFW. REPLACED NR 1 L/E FLAP ACTUATOR AND S202 POSITION SWITCH, OPERATION NORMAL.Jul 15, 1995 · N2826W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72E953080Trunnion Fitting · corrosionLIGHT FRETTING CORROSION ON BORES/CAPS AND FACES OF THE LT/RT TRUNNION FITTINGS. LIGHT CORROSION ON LWD BORE OF LT TRUNNION AFT CAP ATTACH BOLT HOLE. REPAIR PER M/M 53-40-0 FIG 811. FOUND A AT HMV.Jul 15, 1995 · N282WA · Boeing 727247 · Fuselage, Landing Gear Attach FittingsSDR DL72W953096Stringer · corrodedSTRINGER 27L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER. INSTALLED REPAIR PER SRM 53-10-3, FOUND AT HMV.Jul 14, 1995 · N292WA · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W953079Stringer · corrodedAT HMV, STR 27 L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER AS PER B-727 SRM 53-10-3.Jul 14, 1995 · N292WA · Boeing 727247 · Fuselage Main, Longeron/StringerSDR UPS203825Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND BOX FRAME UPPER WEB AT STA 840 RBL 65 CRACKED. REPLACED IAW SRM 51-30-2, M/M 51-20-151, 51-20-21.Jul 12, 1995 · N207UP · Boeing 727247 · Fuselage Main, FrameSDR DL72W953032Rib · crackedNR 3 SLAT RIB CRACKED, I/B OF ACTUATOR ATTACH POINT CRACKED IN RADIUS AT LOWER AFT END OF RIB. INSTALLED DOUBLER PER MM 57-54-0 PG 819. FOUND AT HMV.Jul 10, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72E953067Tire · failedDURING CRUISE, A LOUD NOISE WAS HEARD IN CABIN. RETURNED TO ATL. THE RIGHT GEAR NR 3 TIRE HAD THE RETREAD BLOW OFF. DAMAGE OCCURED TO APU EXHAUST DUCT, GEAR DOOR RELEASE BRACKETS, L/E OF NR 3 PYLON AND RIGHT INBD AFT FLAP. WHEN WHEEL ASSEMBLY WAS CHANGED IJul 10, 1995 · N830WA · Boeing 727247 · TireSDR DL72W953005Overheat Loop · cutAT FL 270, 25 MIN INTO FL, LOWER AFT BODY O/H LIGHT ILLUM INTERMITTENTLY FOR APPROX 1 MIN, THEN STEADY. C/W POM PROC AND LIGHT REMAINED ILLUM FOR 15 TO 20 MIN WITH NR 2 THROTTLE AT IDLE. AFTER 20 MIN WITH NR 2 THROTTLE AT IDLE LIGHT EXT WITH A COUPLE OF FLICJul 9, 1995 · N2821W · Boeing 727247 · Overheat DetectionSDR DL72W953149Angle · crackedCRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA302097-14AD.Jul 8, 1995 · N2809W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W953006Rib · crackedITEM: NR 6 SLAT RIB CRACKED AT RIVET FWD FLANGE OF RIB NR 7. CORRECTION: REPAIRED PER S.R.M. 57-50-03, FIG 09. DAMAGE FOUND AT HMV.Jul 8, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72W952986Controller · faultyDURING CRUISE, AT FL 250 WITH SINGLE PACK OPERATION HAD CABIN ALTITUDE HORN. INITIATED EMERGENCY DESCENT, LANDED BOS. REPLACED LEFT PACK 35 DEG CONTROLLER, PACK OPERATION NORMAL.Jul 8, 1995 · N2812W · Boeing 727247 · Cabin Cooling SystemSDR DL72W953001Skin · damagedAT HMV, FOUND NR 4 SLAT INNER ANTI-ICE SKIN BETWEEN NR 12, NR 13 RIBS HAS HOLE. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, FIG 803A.Jul 7, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72W953000Angle · crackedAT HMV, FOUND NR 4 SLAT ATTACH ANGLE ABOVE NR 13 RIB CRACKED. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, PG 807.Jul 7, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72W952965Skin · crackedNR 6 SLAT SKIN CRACKED AT TAB FOR INBD TRACK FAIRING ATTACH. INSTALLED REPAIR PER MM 57-54-0, PG 820/821. FOUND AT HMV.Jul 6, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72W953137Skin · wornNR 3 AFT FLAP L/E SKIN WORN AT 21 AND 35 FROM O/B END OF FLAP. REPAIRED PER SRM 57-50-4, FOUND AT SHOP INSPECTION.Jul 5, 1995 · N296WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W952934Bracket · crackedBRACKETS CRACKED, NR 2 KRUEGER FLAP ACTUATOR, O/B SUPPORT BRACKET AND I/B SUPPORT BRACKET. DYE CHECKED, FOUND NO DISCREPANCIES PER PS 900-6-301.Jul 5, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72W952932Ribs · crackedAT HMV, FOUND NR 4 L/E SLAT WITH RIB NR 1, 10, 13, 15 CRACKED. REPAIRED CRACKED RIBS PER MM 57-54-0.Jul 5, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72W953151Angle · crackedCRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA 302068-14AD.Jul 4, 1995 · N2807W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W952933Angle · crackedAT HMV, NR 4 SLAT ANGLE FOR CLOSEOUT PANEL CRACKED AT FWD LOWER EDGE AT RIB NR 12 AND NR 13. REPAIRED PER MM 57-54-0.Jul 4, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR UPS203747Skin · crackedWHILE ON GROUND IN ST. PETERSBURG, FL, MAINTENANCE FOUND NR 10 SPOILER HAS 12 INCH CRACK IN TOP PANEL. REPLACED IAW M/M 27-61-01.Jul 3, 1995 · N209UP · Boeing 727247 · SpoilersSDR DL72W952916Skin · crackedRT ELEVATOR LWR SKIN CRACKED 1 INCH AT L/E AFT OF NR 4 BALANCE BOARD. FOUND AT C-1 LTR CK. REPAIRED PER SRM 55-20-3 FIG 4.Jul 3, 1995 · N2807W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W952915Skin · crackedA .5 INCH CRACK RT ELEVATOR LWR SKIN AFT OF NR 4 BALANCE BOARD. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 55-20-3 FIG 4.Jul 3, 1995 · N2807W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W952914Skin · corrodedSKIN CORRODED AT STA 720C STR 10 RT. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 53-30-3 FIG 5, TIME LIMITED DOUBLER.Jul 3, 1995 · N2807W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W952913Skin · corrodedFOUND A LINE OF SMALL NICKS 6 INCHES LONG COMING DOWN FROM AFT LAV SERVICE PAN ON THE FUSELAGE SKIN WITH CORROSION. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 53-30-1, FOUND IN ALLOWABLE LIMITS.Jul 3, 1995 · N2807W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W953009Hyd Hose · leakingON GEAR RETRACTION, HAD LOSS OF A-SYSTEM HYD QTY AND PRESS. RETURNED SLC. FOUND LINE TO LEFT ELEVATOR ACTUATOR CRACKED. REPLACED LINE, OPERATION NORMAL.Jul 2, 1995 · N297WA · Boeing 727247 · Hydraulic System, MainSDR DL72W952937Seat Track · corrodedAT HMV, SEAT TRACK CORRODED, FROM FS 1070-1110 RT IB TRACK RBL 24.5. REMOVED CORROSION PER SRM 51-10-06. REPLACED TRACK FROM FS 1070 TO 1110 PER MM 53-20-11, PG 806.Jul 2, 1995 · N292WA · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR DL72W952930Seal · failedON CLIMBOUT, HAD RT PACK FAILURE LEFT PACK UNABLE TO MAINTAIN PRESSURE. EMERGENCY DESCENT WAS MADE, LANDED ATL. FOUND HULL SEAL CENTER TANK AND FWD CARGO JUNCTION DISPLACED AND TORN. REPAIRED SEAL AND REPLACED RT PACK CONTROL VALVE, OPERATION NORMAL.Jul 1, 1995 · N2820W · Boeing 727247 · Cabin Pressure Control SystemSDR DL72W952866Skin · holeAT HMV SHOP INSPECTION OF NR 1 F/F, WORN AREA FOUND 11 TO 12 INCHES FORM I/B END OF FLAP. ACCOMPLISHED REPAIRS PER SRM 57-50-4.Jun 30, 1995 · N292WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W952865Le Skin · wornAT HMV SHOP INSPECTION, NR 1 FOREFLAP FOUND WITH A HOLE IN THE L/E 10.5 INCHES FROM I/B END. REPAIRED PER SRM 57-50-4.Jun 30, 1995 · N292WA · Boeing 727247 · Trailing Edge Flaps
Back to Boeing 727-247