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 DL72E951064Stringer · corrodedAT HMV, FOUND STR 28R CORRODED AT SPLICE AT FS 1050. REPAIRED PER SRM 53-10-3.Feb 27, 1995 · N2823W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72E951063Skin · corrodedAT HMV, FOUND AFT B/B FUSELAGE SKIN WITH CORROSION DAMAGE UNDER A PREVIOUS REPAIR AT FS 1065 AT STR 28L. REPAIRED PER SRM 53-30-3.Feb 27, 1995 · N2823W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E951061Skin · crackedAT HMV, FOUND FUSELAGE SKIN CRACKED AT FS 700 AT STR 26L. REMOVED DAMAGED AREA, REPAIRED PER SRM 53-30-3.Feb 27, 1995 · N2823W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E951021Skin · crackedNR 6 LE SLAT INTERIOR SKIN CRACKED, LOCATED IN BAY IB OF ACTUATOR RIBS. REPAIRED PER MM 57-54-0 PG 804. FOUND AT HMV.Feb 27, 1995 · N2823W · Boeing 727247 · Leading Edge DevicesSDR DL72E951000Stringer · crackedDURING HMV FOUND L/W L/E LIGHT BOX, STR 15L IS CRACKED ON FWD AND AFT SIDES OF LIGHT BOX, REPAIRED PER SRM 53-10-3 FIG 1 DETAIL II FOR FWD AND AFT.Feb 27, 1995 · N2823W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72E950999Ribs · crackedDURING HMV FOUND NR 4 LEADING EDGE SLAT RIB MARKED NR 21 CRACKED AT FWD CLOSURE CHORD, REPAIRED PER M/M 57-54-0 PG 806.Feb 27, 1995 · N2823W · Boeing 727247 · Leading Edge DevicesSDR DL72E950998Ribs · crackedDURING HMV FOUND NR 4 SLAT ACTUATOR RIB MARKED NR 12 CRACKED 3 PLACES AND RIB MKD NR 11 CRACKED IN FWD LOWER RADIUS, REPAIRED PER M/M 57-54-0 PG 805.Feb 27, 1995 · N2823W · Boeing 727247 · Leading Edge DevicesSDR DL72E950983Rib · crackedDURING HMV, FOUND NR 6 LEADING EDGE SLAT RIB MARKED '11' IS CRACKED BEHIND CLOSURE CHORD. REPAIRED PER MM 57-54-0.Feb 27, 1995 · N2823W · Boeing 727247 · Leading Edge DevicesSDR DL72E950982Rib · crackedDURING HMV, FOUND NR 6 LEADING EDGE SLAT TAI 'T' DUCT HAS EXCESSIVE PLAY AT 'T' JOINT. THE ADJACENT O/B RIB TO ABOVE BAY IS CRACKED AT FWD CLOSURE CHORD. REPAIRED PER MM 57-54-0 PG 806.Feb 27, 1995 · N2823W · Boeing 727247 · Leading Edge DevicesSDR DL72E950981Rib · crackedDURING HMV, FOUND NR 1 LEADING EDGE SLAT RIB MARKED NR 4 HAS CRACKED ATTACH ANGLE. REPAIRED BY REPLACING ANGLE.Feb 27, 1995 · N2823W · Boeing 727247 · Leading Edge DevicesSDR DL72E950935Stringer · crackedAT HMV, FOUND STRINGER 15R CRACKED AT ITS ENDS AT WING ICE LIGHT HOUSING FS 720C. REPAIRED PER SRM 53-1-03.Feb 27, 1995 · N2823W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72E950899Stringer · crackedAT HMV, AFT SIDE OF FORWARD VENT BOX STRINGER CRACKED AT RIB ATTACH, WS 686.5, LT WING. REPAIRED PER MM 57-13-0 PG 808.Feb 27, 1995 · N2823W · Boeing 727247 · Wing, Longeron/StringerSDR DL72E950892Nose Cowl · wornNOSE COWL, FLANGE WORN, NR 1 ENG NOSE COWL AFT FLANGE IS WORN TO RAZOR EDGE AT 7:00 POSITION. INSTALLED DOUBLER PER SRM 54-10-3. NR 290.Feb 27, 1995 · N2823W · Boeing 727247 · Engine Cowling SystemSDR 95ZZZW205Pin · no installedMIA - AFTER TAKEOFF, THE NLG AND DOOR LIGHT REMAINED ON WITH AIRFRAME VIBRATION AND AIR NOISE FROM GEAR AREA. RETURNED TO MIA. FOUND NOSE GEAR SENSOR LINK PIN NOT INSTALLED. REINSTALLED PIN. REPLACED LT AND RT NLG WHEELS. INSPECTED AREA, ACFT DEPARTED TOFeb 27, 1995 · N326AS · Boeing 727247 · Landing Gear Retraction/Extension SystemSDR DL72E951351Flap · corrodedTHE NR 4 MID FLAP, I/B CARRIAGE THRUST BEARING RETAINER UPPER I/B AND O/B BOLT HOLES CORRODED. REPAIRED PER SRM 57-57-04, REAMED AND BUSHED HOLES. FOUND AT HMV SHOP INSPECTION.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951350Flap · corrodedTHE NR 4 MID FLAP, I/B AND O/B CARRIAGE SUPPORT HOUSING BOTTOM SURFACE EACH HAVE 5 BOLT HOLES CORRODED. REPAIRED PER SRM 57-50-04 REAMED AND BUSHED HOLES. ALSO, I/B HAS 2 DAMAGED SPRING ATTACH BOLT HOLES. REPAIRED PER SRM 57-50-04. REAMED AND BUSHED HOLES.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951135Flap · crackedNR 2 MID FLAP, CRACK IN LOWER AFT SPAR CHORD AT 41 INCHES FROM O/B END OF FLAP AND ONE AT 18 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 575200 PG 807, INSTALLED DOUBLER. FOUND AT HMV SHOP INSPECTION.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951102Flap · wornNR 1 FORE FLAP, LEADING EDGE WORN 12 INCHES FROM I/B END LOWERSIDE. FOUND DURING HMV, SHOP INSPECTION. REPAIRED PER SRM 57-50-4, FIG 1.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951101Flap · damagedNR 1 FORE FLAP, TWO TEMP REPAIRS ON LEADING EDGE NEAR I/B END ON UPPER SIDE OF FLAP. FOUND DURING HMV, SHOP INSP. REPLACED TEMP REPAIRS WITH PERM REPAIR AS PER 57-50-4, FIG 1.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951099Flap · damagedNR 1 FORE FLAP, TEMP REPAIR INSTALLED ON LEADING EDGE, 48 INCHES FROM O/B END. FOUND AT HMV, SHOP INSPECTION. REPAIRED PER SRM 57-50-4, FIG. 1Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951071Doubler · mis installedNR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE IMPROPERLY INSTALLED DOUBLER ON AFT LOWER SPAR AT QUADRANT PUSH ROD CUTOUT I/B END. THIS IS A REWRITE FROM CARD NR 4974.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951069Spar · crackNR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE A CRACKED AFT LOWER SPAR 55 INCHES FROM I/B END.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951062Flap Doubler · mis installedNR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE AN IMPROPERLY INSTALLED DOUBLER ON THE AFT LOWER SPAR AT I/B QUADRENT PUSH ROD CUTOUT.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951060Flap · corrosionNR 3MID FLAP DURING HMV INSP WAS FOUND TO HAVE CORROSION IN THREE THRUST BEARING RETAINER BOLT HOLES.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR DL72E951059Flap · corrosionNR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE CORROSION I/B CARRIAGE FITTING IN THE I/B THRUST BEARING RETAINER BOLT HOLE CORROSION WAS REPAIRED PER SRM 57-50-4.Feb 25, 1995 · N2823W · Boeing 727247 · Trailing Edge FlapsSDR 95ZZZW214Eel Lens · missingRED LENS MISSING FROM EMERGNECY PATH LIGHTING. REPLACED MISSING LENS FOR EMERGENCY PATH LIGHTING. OPS NORMAL.Feb 24, 1995 · N326AS · Boeing 727247 · Emergency LightingSDR DL72E950894Nose Cowl · damagedTWO TEMP REPAIRS LOCATED AT THE 5:00 AND 6:00 POSITIONS IN THE NOSE COWL LIP SKIN. C/W ERA 258540-14 BY INSTALLING DOUBLER PER SRM 54-30-3 FIGURE 2. N/R'S 202 AND 5.Feb 22, 1995 · N2823W · Boeing 727247 · Engine Cowling SystemSDR DL72W950907Spar · crackedDURING SHOP INSPECTION, FOUND NR 2 MIDFLAP AFT LOWER SPAR WITH 2 CRACKS AT 53 INCHES AND 56 INCHES FROM INBD END OF FLAP. REPAIRED PER MM 57-52-20 PG 807.Feb 19, 1995 · N293WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W950659Panel · delaminatedDURING LETTER CHECK, FOUND RT WING SPOILER PANEL WITH DELAMINATION DAMAGE, REPAIRED PER SRM 57-50-6.Feb 17, 1995 · N2816W · Boeing 727247 · SpoilersSDR DL72W950812Angle · crackedDURING INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. THE ANGLE WILL BE REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4.Feb 14, 1995 · N2816W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W950620Angle · crackedFOUND DURING D-2 LETTER CHECK, COVE SKIN ATTACH ANGLE CRACKED 2 INCH AT O/B STOP FITTING NR 6 SLAT. REPAIRED PER MM 57-54-0 PG 816.Feb 14, 1995 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W950618Skin · crackedDURING SHOP INSPECTION, FOUND NR 4 SLAT SKIN CRACKED AT MOUNT HOLE FOR THE WING FENCE. REPAIRED PER MM 57-54-0.Feb 14, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72W950617Te Fairing · crackedDURING SHOP INSPECTION, FOUND NR 4 SLAT WITH THE I/B AND O/B TRACK FAIRINGS CRACKED. REPAIRED PER MM 57-54-0.Feb 14, 1995 · N292WA · Boeing 727247 · Leading Edge DevicesSDR DL72E950610Rib · crackedFOUND CRACKED RIB UPON INSPECTION ON NR 2 SLAT. REPAIRED RIB PER MM 57-54-00.Feb 13, 1995 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72W950643Bulkhead Web · crackedBS 1183 BULKHEAD WEB CRACKED IN 4 PLACES AT RBL18. 1.0 INCH CRACK AT WL173, 0.5 INCH CRACK AT WL175, 1.25 INCH CRACK AT WL177, AND 1.0 INCH CRACK AT WL 179. CRACKS STOP DRILLED AND REPAIR DOUBLER INSTALLED. DAMAGE FOUND DURING LETTER CHECK, REPAIRED PER EARFeb 7, 1995 · N2815W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W950527Skin · crackedDURING SHOP INSPECTION RIGHT WING NR 6 SLAT WAS FOUND WITH A CRACK IN THE LOWER SKIN AT 19 INCH FROM THE INBOARD END OF SLAT AND 13 INCH FROM THE OUTBOARD END OF SLAT. REPAIRED PER SRM 57-54-0.Feb 7, 1995 · N294WA · Boeing 727247 · Trailing Edge FlapsSDR DL72E950529Angle · crackedTHERE IS A 1 INCH CRACK IN THE ANGLE OF THE FORWARD TRANSVERSE BEAM OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER S/B 53-0129. DAMAGE FOUND AT LETTER CHECK.Feb 7, 1995 · N830WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E951172Tee · corrosionAT HMV, FOUND CORROSION AT LOWER FUSELAGE HINGED PANEL 3348 FRAME WHERE HINGES ATTACH, IN THE RADIUS OF FRAME BEAM. REPAIRED ATTACH 'T' PER M/M 53-30-1, REPAIRED FORMED SECTION PER SRM 51-40-3 FIG 1.Feb 6, 1995 · N2823W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W950577Detector Unit · failedON CLIMB-OUT, NR 1 ENGINE STRUT OVERHEAT ILLUMINATED, UNABLE TO EXTINGUISH, SHUT DOWN NR 1 ENGINE. REPLACED DETECTOR UNIT, SECURED DUCT CLAMP AT 13TH STAGE VALVE, RETURNED TO SERVICE.Feb 5, 1995 · N2822W · Boeing 727247 · Overheat DetectionSDR DL72E950758Spar · crackedDURING INSPECTION, THE RIGHT ELEVATOR REAR SPAR WAS FOUND TO HAVE A CRACK EMANATING .1250 INCH FROM THE INBD SIDE OF THE SHEAR PLATE AT THE SECOND FROM THE OUTBD TAB HINGE FITTING TO REAR SPAR ATTACHMENT. THE CRACK WAS STOP DRILLED IN ACCORDANCE WITH B727 S/BFeb 3, 1995 · N830WA · Boeing 727247 · Elevator, Spar/RibSDR DL72W950759Stringer · crackedDURING INSPECTION AT OVERHAUL, STRINGER 7R OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FIN STA 110.4 RIB ATTACHMENT TAB. IN ACCORDANCE WITH B727 S/B 55-0075, A REPAIR ANGLE WAS INSTALLED.Feb 2, 1995 · N293WA · Boeing 727247 · Vertical StabilizerSDR DL72E950492Former · crackedFOUND ON C2 LETTTR CHECK, FWD COWL TO FUSELAGE LIP DAMAGED AT 6 O'CLOCK POSITION, REPAIR AND REPLACED DOUBLER PER M/M 53-11-0 PG 801Feb 2, 1995 · N830WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E950491Web · crackedFOUND ON C2 LETTER CHECK, TWO .25 INCH CRACKS UPPER LIGHTENING HOLE STA 1240R - AFT STAIRWELL AREA, REPAIRED PER 53-11-0 NR 15.Feb 2, 1995 · N830WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS202159Eel · inoperativeMAINTENANCE REPORTED EXIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY.Feb 1, 1995 · N210UP · Boeing 727247 · Emergency LightingSDR DL72W950465Rib · crackedDURING HMV, FOUND RIB CHORD CRACKED AT FIN STA 110 AT STR 10 LEFT. REPAIRED PER MM 55-30-0 PG 802.Feb 1, 1995 · N293WA · Boeing 727247 · Vertical Stabilizer, Spar/RibSDR DL72W950464Stringer · crackedDURING HMV, STR 9 LEFT INSIDE VERT STAB AT FIN STA 110 CRACKED. REPAIRED PER MM 55-30-0 PG 803 FIG 803.Feb 1, 1995 · N293WA · Boeing 727247 · Vertical StabilizerSDR DL72W950487Stringer · crackedFOUND DURING HMV, NR 5 STR CRACKED INSIDE VERT STAB AT STA 110.4. REPAIRED PER ERA 301113-14.Jan 30, 1995 · N293WA · Boeing 727247 · Vertical StabilizerSDR DL72W950486Attach Angles · crackedFOUND DURING HMV, ATTACH ANGLE CRACKED AT NR 5 STR ABOVE NR 2 'S' DUCT INSIDE VERT STAB. REPAIRED PER SRM55-30-5 PG.1, FIG 1.Jan 30, 1995 · N293WA · Boeing 727247 · Vertical StabilizerSDR DL72W950413Panel · dentedDURING SHOP INSPECTION, RT WING SLAT PANEL WAS FOUND WITH DENTED UPPER SKIN. REPAIRED PER SRM 57-50-3 FIG 1.Jan 29, 1995 · N293WA · Boeing 727247 · Leading Edge DevicesSDR DL72W950406Rib · crackedDURING SHOP INSPECTION, FOUND NR 6 RIB FOR NR 3 SLAT CRACKED. REPAIRED PER SRM 57-54-0.Jan 29, 1995 · N2807W · Boeing 727247 · Leading Edge Devices
Back to Boeing 727-247