N275WC, cancelled Mar 6, 2017

Service difficulty reports · 65

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N275WC' AND deregistration_id = 'N275WC-2017-03-06'
  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 EISA20010147Pin · misinstalledGOT UNSAFE NOSE GEAR DOOR LIGHT ON CLEANUP RTB. ON LANDING, HAD SEVERE VIBRATION WHEN NOSE WHEEL LOWERED TO GROUND.CORRECTIVE ACTION:FOUND NLG APEX PIN IMPROPERLY INSTALLED. INSTALLED PIN PER MM 32-21.(SUBSEQUENT D.V.I. OF NLG AND DOORS & W/W FOUND NO DEFECTSDec 17, 2001 · N275WC · Boeing 727277 · Landing Gear Steering SystemSDR EISA20010108Engine · inoperative#1 ENG LOSING OIL QTY, OIL TEMP ON THE RISE, LOSING OIL PRESS. ENGINE #1 SHUT DOWN.CORRECTIVE ACTION:#1 ENGINE TO BE REMOVED.Jul 21, 2001 · N275WC · Boeing 727277 · Engine Oil QuantitySDR EISA20010077Static Line · looseAIRCRAFT LOST CABIN PRESSURE ON CLIMBOUT. AIR TURNBACK. SECURED STATIC LINE TO PRESSURE CONTROLLER IAW M/M 31-30-0. REPLACED DAMAGED WIRE SPLICE TO FLOW CONTROL RELAY IN E-4 POWER SHIELD PER M/M 21-00 & 20-30-22.Apr 30, 2001 · N275WC · Boeing 727277 · Cabin Pressure Control SystemSDR EISA20010076Wire · damagedAIRCRAFT LOST PRESSURE AT FL 250, AIR TURNBACK TO IND. REMOVED AND REPLACED 13TH STAGE MOD VALVE PER M/M 36-12, NO HELP ITEM REMAINS OPEN. FERRIED AIRCRAFT FOR MAINT. FOUND DAMAGED WIRE SPLICE IN E-4 POWER SHEILD. REPAIRED PER M/M 21, OPS CHECK NORMAL.Apr 24, 2001 · N275WC · Boeing 727277 · Air Conditioning System WiringSDR EISA20010034Fitting · looseINFLIGHT NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. ASSOCIATED PRESSURE INDICATED 10-12 PSI. ENGINE SHUT DOWN IAW EXPRESS ONE CHECKLIST, DIVERTED INTO OMA. REPLACED GEARBOX FITTING TO DIFFERENTIAL PRESSURE PORT IAW 72-61-00. NO DEFECTS NOTED.Mar 2, 2001 · N275WC · Boeing 727277 · Turbine Engine Accessory DriveSDR EISA20000232Switch · malfunctionedGOING THROUGH 13000 FT LEADING EDGE FLAP AMBER LIGHT RE-ILLUMINATED ON REAR PANEL SHOWED NR 3 LEADING EDGE FLAP LIGHT INTRANSIT. REMOVED AND REPLACED NR 3 SWITCH.Dec 29, 2000 · N275WC · Boeing 727277 · Leading Edge Slat Position Indicating SystemSDR EISA20000225Skin · puncturedPUNCTURE AT NR 2 ENGINE NOSE COWL AFT OF INLET RING. CORRECTIVE ACTION: CUT OUT PUNCTURED SKIN, FABRICATED, FILLER, AND DOUBLER, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-10-2, 51-40-2 FIG. 1, 54-30-3 FIG.5, 54-30-2, 51-30-2.Nov 16, 2000 · N275WC · Boeing 727277 · Nacelle/Pylon, Plate/SkinSDR EISA20000224Skin · gougedNR 3 AFT FLAP GOUGED AND WORN THRU TO HONEYCOMB IN SEVERAL PLACES. CORRECTIVE ACTION: POTTED CORE, CLEANED, PREPPED, BONDED FIBERGLASS OVERLAYS, ALODINED, PRIMED, AND PAINTED IAW SRM 51-40-6 FIG. 35, 51-10-2, M/M 27-50-2, 51-20-71, 51-20-151.Nov 16, 2000 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA20000223Skin · gougedNR 3 AFT FLAP GOUGED IN SEVERAL PLACES. CORRECTIVE ACTION: POTTED CORE AREA, CLEANED, PREPPED, BONDED FIBERGLASS OVERLAYS, ALODINED, PRIMED, AND PAINTED IAW SRM 51-40-6 FIG. 35, 51-10-2, M/M 51-20-151 AND 51-20-71.Nov 16, 2000 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA20000222Skin · dentedSMALL DENT ON TOP SKIN AFT FLAP. CORRECTIVE ACTION: REMOVED DENTED AREA, POTTED CORE, CLEANED, PREPPED, BONDED FIBERGLASS OVER LAYS, ALODINED, PRIMED, AND PAINTED IAW SRM 51-40-6 FIG. 35, 51-10-2, AND M/M 51-20-151.Nov 16, 2000 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA20000136Module · malfunctionedNR 3 LEADING EDGE FLAP LIGHT ILLUMINATED IN FLIGHT. AFTER LANDING UPON FLAP RETRACTION LIGHT WENT OUT. UNSCHEDULED LANDING AT PHX. OPS CHECK NR 3 LEADING EDGE FLAP LIGHT. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME IAW M/M 27-80.Sep 6, 2000 · N275WC · Boeing 727277 · Trailing Flap Position Indicating SystemSDR EISA2000049Switch · out of adjDURING CRUISE AT FL 28,000 FT, MAIN CARGO DOOR UNLOCKED LIGHT ILLUMINATED. AT FL 20,000 FT, THE SAME LIGHT EXTINGUISHED (RETURN TO IND FLIGHT 6171). ADJUSTED AFT SIDE LOCK SWITCH, S-15. PRESSURIZED TO 8.2 PSI PUSHED ON DOOR LIGHT, DID NOT ILLUMINATE AGAIN. May 12, 2000 · N275WC · Boeing 727277 · Door Warning SystemSDR EISA2000032Landing Gear · lack of lubeEXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF. RETURNED TO BLOCKS (SLC). LUBED NOSE GEAR AND SERVICED NOSE TIRES. (M)Mar 15, 2000 · N275WC · Boeing 727277 · Nose/Tail Landing GearSDR EISA99128Excitor · inoperativeNR 3 ENGINE WOULD NOT LIGHT OFF. REMOVED AND REPLACED NR 3 ENGINE IGNITION EXCITOR. (M)May 20, 1999 · N275WC · Boeing 727277 · ExciterSDR EISA98316Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FIVE AREAS OF DELAMINATION ON LEFT OUTBOARD AFT FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-06, ALUMINUM HONEYCOMB REPAIR. (M)Dec 9, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98315Skin · dentedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DENT ON LOWER SURFACE ON LEFT OUTBOARD AFT FLAP. REPAIRED DENT PER SRM 51-40-6, ALUMINUM HONEYCOMB. (M)Dec 9, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98314Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TWO RIBS AND ONE BRACKET CRACKED IN STRUCTURE OF E/E DOOR. REMOVED DAMAGED RIBS AND BRACKET. FABRICATED AND INSTALLED NEW RIBS AND BRACKET PER SRM 52-40-1 AND 51-30-2. (M)Dec 9, 1998 · N275WC · Boeing 727277 · Electrical/Electronic Compartment DoorsSDR EISA98309Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 8 SLAT WAS FOUND CRACKED AT MOST OUTBOARD RIB. FABRICATED DOUBLER REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-3. (M)Dec 9, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR EISA98319Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD , FOUND TWO AREAS OF DELAMINATION ON RIGH OUTBOARD AFT FLAP TRAILING EDGE. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-05, ALUMINUM HONEYCOMB REPAIR. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98318Skin · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND GOUGES ON UPPER SURFACE OF RIGHT OUTBOARD AFT FLAP. REPAIRED THREE GOUGES PER SRM 51-40-6 ALUMINUM HONEYCOMB REPAIR. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98317Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND AREA OF DELAMINATION ON OUTBOARD END OF LEFT INBOARD AFT FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-5, BONDED METAL REPAIR. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98313Angle · corrodedDURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-1 CORROSION WAS FOUND TO EXIST ON FWD LAV BULKHEAD INSTALLATION ANGLE, RBL 16 AND 8 INCHES AFT OF FLT DECK THRESHOLD. REMOVED CORROSION FROM FWD LAV BULKHEAD. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2.Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Miscellaneous StructureSDR EISA98312Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 2 SLAT WAS DISCOVERED CRACKED AT THIRD RIB FROM INBOARD END. FABRICATED DOUBLER REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR EISA98311Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 3 SLAT WAS FOUND CRACKED AT 2ND AND 7TH RIBS FROM OUTBOARD END. FABRICATED DOUBLER REPAIRS PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR EISA98310Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 5 SLAT WAS FOUND CRACKED AT NR 5 AND NR 9 RIBS FROM INBOARD END. FABRICATED DOUBLER REPAIRS PER SRM 51-50-2 AND INSTALLED PER SRM 57-20-3. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR EISA98307Skin · crackedDURNG ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, X-RAY INSPECTION OF LEFT ELEVATOR SHOWS CRACK INDICATION OF .25 INCH AS SEEN IN SHOT NR L06, STATION 17.20-53.91). REMOVED LEFT ELEVATOR TAB TO FOM REPAIRED CRACK IN ELEVATOR PER SRM 51-40-3. ACCOMPLISHED BADec 8, 1998 · N275WC · Boeing 727277 · Elevator, Plate/SkinSDR EISA98306Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD NR C53-224-01 REVEALED CORROSION ON UPPER CHORD OF FS 1070 FLOORBEAM RBL 55. REMOVED DAMAGED SECTION OF UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98302Bulkhead · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FS 178 BULKHEAD CRACKED, JUST BELOW RADAR ANTENNA. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER B727 SB 53-0213. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, BulkheadSDR EISA98301Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD C53-224-01, NINE SMALL AREAS OF DELAMINATION ON RIGHT INBOARD AFT FLAP. REPAIRED ALL AREAS PER SRM 51-40-6. ALUMINUM HONEYCOMB REPAIRS. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98300Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-01 REVEALED TWO MAIN AREAS OF CORROSION ON UPPER CHORD OF FS 1110 FLOORBEAM. REMOVED DAMAGED AREAS. FABRICATED AND INSTALLED REPAIRS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98299Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-01 REVEALED CORROSION ON IN TWO AREAS OF UPPER CHORD OF FLOORBEAM FS 1030. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98297Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND AREA WITH GOUGED AND CRACKED SKIN ON UPPER SURFACE OF RIGHT INBOARD AFT FLAP. REMOVED DAMAGED SKIN. FABRICATED AND INSTALLED NEW SKIN SECTION PER SRM 57-50-4. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98293Floorbeam · corrodedDURING C-CHECK ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED FOUR AREAS OF CORROSION ON T-CAP OF FLOORBEAM AT FS 328. REMOVED DAMAGED AREAS AND INSTALLED REPAIRS PER SRM 53-10-8 AND 51-30-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98292Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON FLOORBEAM AT FS 400 LBL 45. TRIMMED DAMAGED UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-02. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98291Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON UPPER CHORD OF FLOORBEAM AT FS 440 LBL 25. TRIMMED DAMAGED AREA OF UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-1. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98290Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED THREE AREAS OF CORROSION ON FLOORBEAM AT FS 400. TRIMMED AREAS OF DAMAGED CHORD. FABRICATED AND INSTALLED REPAIRS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98289Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON FLOORBEAM UPPER CHORD AT FS 680. REMOVED DAMAGED AREA OF UPPER CHORD FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR EISA98288Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND THREE AREAS OF DELAMINATION ON RIGHT INBOARD MID FLAP TRAILING EDGE. REPAIRED AREAS PER SRM 51-40-6 ALUMINUM HONEYCOMB REPAIR. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98287Skin · puncturedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND SKIN PUNCTURE ON RIGHT INBOARD MID FLAP TRAILING EDGE LOWER SIDE. REPAIRED SKIN PUNCTURE PER SRM 51-40-6, 51-40-8, AND 51-40-9. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98286Frame · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CRACK IN FRAME AT FS 580 AND STRINGER 7R. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-4. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, FrameSDR EISA98285Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TWO AREAS OF DELAMINATION ON LEFT INBOARD MID FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-6 AND 51-40-8. (M)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR EISA98242Sensor · malfunctionedCAUTION LIGHT ILLUMINATED ON F/E PANEL FOR MAIN CARGO DOOR DURING FLIGHT. AIR TURN BACK TO BSL. INSPECTED CARGO DOOR PER PEMCO MM 52-32-23. FOUND ALL OPS INDICATORS NORMAL. (M)Oct 1, 1998 · N275WC · Boeing 727277 · Door Warning SystemSDR EISA98204Skin · crackedDURING ACCOMPLISHMENT OF CPCP CARD C53-100-01 PART 4 INSPECTION OF LOWER FUSE BS 178 TO 1183. DETECTED ROW OF RIVETS RIGHT SIDE AT STRINGER 25 STATION 680 TO 660 SKIN BULGED AND STRINGER CRACKED WITH CORROSION. REPLACED STRINGER 25 PER SRM 53-10-3 FIG 1 HEAVAug 1, 1998 · N275WC · Boeing 727277 · Fuselage Main, Plate/SkinSDR EISA98184Stringer · crackedDURING ACCOMPLISHMENT OF CPCP CARD C 53-100-01 PART 4 INSPECTION OF LOWER FUSE BS 178 TO BS 1183, DETECTED ROW OF RIVETS RIGHT-HAND SIDE AT S25 STA 680 TO STA 660, SKIN BULGED AND STG CRACKED WITH CORROSION. CORRECTIVE ACTION: REPLACED STG 25 PER SRH 53-10-0Aug 1, 1998 · N275WC · Boeing 727277 · Fuselage Main, Longeron/StringerSDR EISA98183Connector · looseRETURNED TO BRU DUE TO PRESSURIZATION INOPERATIVE. GENERATED FROM PILOT REPORT. CORRECTIVE ACTION: TROUBLESHOT AND FOUND CONNECTOR TO OUTFLOW VALVE LOOSE. RESECURED CONNECTOR SYSTEM. CHECKS GOOD. MM CHAPTER 21. (X)Jul 27, 1998 · N275WC · Boeing 727277 · Pressure Regulator/Outflow ValveSDR EISA98066Vhf Com · intermittentAFTER TAKEOFF FROM BRU, NR 1 COM WORKED INTERMITTENTLY. AIR TURN BACK TO BRU. PERFORMED NR 1 VHF ANTENNA BONDING CHECK PER MM 23. NO DEFECTS FOUND. ANTENNA COAX AND ANTENNA RESISTANCE NORMAL. REMOVED AND REPLACED NR 1 VHF. (M)Mar 23, 1998 · N275WC · Boeing 727277 · VHF Communications SystemSDR EISA97227Connector · looseON CLIMB-OUT AT BGY F/OS AIRSPEED INDICATOR DECREASED TO ZERO, ON APPROACH INDICATOR BEGAN TO CLIMB BUT NEVER REACHED NORMAL INDICATION. FOUND PITOT CONNECTION LOOSE ON F/O AIRSPEED INDICATOR. RESECURED CONNECTION. PITOT LEAK CHECK GOOD MM 34-11-0. (M)Nov 23, 1997 · N275WC · Boeing 727277 · Airspeed/Mach IndicatorSDR EISA97142Fire Loop · inoperativeNR 3 FIRE WARNING WOULD NOT TEST. REMOVED AND REPLACED FIRE LOOP, REPAIRED WIRING TO CONNECTOR. (M)Jun 17, 1997 · N275WC · Boeing 727277 · Fire DetectionSDR EISA95289Connector · damagedGEAR HANDLE WOULD NOT RETRACT PAST 'OFF' POSITION ON DEPARTURE. STRAIGHTENED PIN NR 24 ON D4654P PLUG. OPS CHECKS GOOD IAW MM 32-09-121. (M)Sep 18, 1995 · N275WC · Boeing 727277 · Landing Gear SelectorSDR EISA95288Skin · delaminationLEFT INBOARD FORE FLAP LEADING EDGE SKIN DELAMINATED. REPAIRED FLAP PER SRM 57-50-4 AND SRM 51-60-6. (M)Sep 14, 1995 · N275WC · Boeing 727277 · Trailing Edge Flaps
Back to N275WC, cancelled Mar 6, 2017