# Service difficulty reports: N275WC, cancelled Mar 6, 2017

A list on [N275WC, cancelled Mar 6, 2017](https://openairdocs.org/deregistered/N275WC-2017-03-06.md).

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

Page 1 of 2 · 65 reports

- [SDR EISA20010147](https://openairdocs.org/sdr/EISA20010147.md): Pin · misinstalled · Dec 17, 2001 · N275WC · Boeing 727277 · Landing Gear Steering System
  > GOT 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 DEFECTS
- [SDR EISA20010108](https://openairdocs.org/sdr/EISA20010108.md): Engine · inoperative · Jul 21, 2001 · N275WC · Boeing 727277 · Engine Oil Quantity
  > #1 ENG LOSING OIL QTY, OIL TEMP ON THE RISE, LOSING OIL PRESS. ENGINE #1 SHUT DOWN.CORRECTIVE ACTION:#1 ENGINE TO BE REMOVED.
- [SDR EISA20010077](https://openairdocs.org/sdr/EISA20010077.md): Static Line · loose · Apr 30, 2001 · N275WC · Boeing 727277 · Cabin Pressure Control System
  > AIRCRAFT 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.
- [SDR EISA20010076](https://openairdocs.org/sdr/EISA20010076.md): Wire · damaged · Apr 24, 2001 · N275WC · Boeing 727277 · Air Conditioning System Wiring
  > AIRCRAFT 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.
- [SDR EISA20010034](https://openairdocs.org/sdr/EISA20010034.md): Fitting · loose · Mar 2, 2001 · N275WC · Boeing 727277 · Turbine Engine Accessory Drive
  > INFLIGHT 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.
- [SDR EISA20000232](https://openairdocs.org/sdr/EISA20000232.md): Switch · malfunctioned · Dec 29, 2000 · N275WC · Boeing 727277 · Leading Edge Slat Position Indicating System
  > GOING 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.
- [SDR EISA20000225](https://openairdocs.org/sdr/EISA20000225.md): Skin · punctured · Nov 16, 2000 · N275WC · Boeing 727277 · Nacelle/Pylon, Plate/Skin
  > PUNCTURE 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.
- [SDR EISA20000224](https://openairdocs.org/sdr/EISA20000224.md): Skin · gouged · Nov 16, 2000 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > NR 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.
- [SDR EISA20000223](https://openairdocs.org/sdr/EISA20000223.md): Skin · gouged · Nov 16, 2000 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > NR 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.
- [SDR EISA20000222](https://openairdocs.org/sdr/EISA20000222.md): Skin · dented · Nov 16, 2000 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > SMALL 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.
- [SDR EISA20000136](https://openairdocs.org/sdr/EISA20000136.md): Module · malfunctioned · Sep 6, 2000 · N275WC · Boeing 727277 · Trailing Flap Position Indicating System
  > NR 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.
- [SDR EISA2000049](https://openairdocs.org/sdr/EISA2000049.md): Switch · out of adj · May 12, 2000 · N275WC · Boeing 727277 · Door Warning System
  > DURING 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.
- [SDR EISA2000032](https://openairdocs.org/sdr/EISA2000032.md): Landing Gear · lack of lube · Mar 15, 2000 · N275WC · Boeing 727277 · Nose/Tail Landing Gear
  > EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF. RETURNED TO BLOCKS (SLC). LUBED NOSE GEAR AND SERVICED NOSE TIRES. (M)
- [SDR EISA99128](https://openairdocs.org/sdr/EISA99128.md): Excitor · inoperative · May 20, 1999 · N275WC · Boeing 727277 · Exciter
  > NR 3 ENGINE WOULD NOT LIGHT OFF. REMOVED AND REPLACED NR 3 ENGINE IGNITION EXCITOR. (M)
- [SDR EISA98316](https://openairdocs.org/sdr/EISA98316.md): Skin · delaminated · Dec 9, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98315](https://openairdocs.org/sdr/EISA98315.md): Skin · dented · Dec 9, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98314](https://openairdocs.org/sdr/EISA98314.md): Rib · cracked · Dec 9, 1998 · N275WC · Boeing 727277 · Electrical/Electronic Compartment Doors
  > DURING 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)
- [SDR EISA98309](https://openairdocs.org/sdr/EISA98309.md): Rib · cracked · Dec 9, 1998 · N275WC · Boeing 727277 · Leading Edge Devices
  > DURING 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)
- [SDR EISA98319](https://openairdocs.org/sdr/EISA98319.md): Skin · delaminated · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98318](https://openairdocs.org/sdr/EISA98318.md): Skin · gouged · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98317](https://openairdocs.org/sdr/EISA98317.md): Skin · delaminated · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98313](https://openairdocs.org/sdr/EISA98313.md): Angle · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR EISA98312](https://openairdocs.org/sdr/EISA98312.md): Rib · cracked · Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge Devices
  > DURING 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)
- [SDR EISA98311](https://openairdocs.org/sdr/EISA98311.md): Rib · cracked · Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge Devices
  > DURING 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)
- [SDR EISA98310](https://openairdocs.org/sdr/EISA98310.md): Rib · cracked · Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge Devices
  > DURING 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)
- [SDR EISA98307](https://openairdocs.org/sdr/EISA98307.md): Skin · cracked · Dec 8, 1998 · N275WC · Boeing 727277 · Elevator, Plate/Skin
  > DURNG 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 BA
- [SDR EISA98306](https://openairdocs.org/sdr/EISA98306.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98302](https://openairdocs.org/sdr/EISA98302.md): Bulkhead · cracked · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Bulkhead
  > DURING 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)
- [SDR EISA98301](https://openairdocs.org/sdr/EISA98301.md): Skin · delaminated · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98300](https://openairdocs.org/sdr/EISA98300.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98299](https://openairdocs.org/sdr/EISA98299.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98297](https://openairdocs.org/sdr/EISA98297.md): Skin · cracked · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98293](https://openairdocs.org/sdr/EISA98293.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98292](https://openairdocs.org/sdr/EISA98292.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98291](https://openairdocs.org/sdr/EISA98291.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98290](https://openairdocs.org/sdr/EISA98290.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98289](https://openairdocs.org/sdr/EISA98289.md): Floorbeam · corroded · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR EISA98288](https://openairdocs.org/sdr/EISA98288.md): Skin · delaminated · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98287](https://openairdocs.org/sdr/EISA98287.md): Skin · punctured · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98286](https://openairdocs.org/sdr/EISA98286.md): Frame · cracked · Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Frame
  > DURING 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)
- [SDR EISA98285](https://openairdocs.org/sdr/EISA98285.md): Skin · delaminated · Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > DURING 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)
- [SDR EISA98242](https://openairdocs.org/sdr/EISA98242.md): Sensor · malfunctioned · Oct 1, 1998 · N275WC · Boeing 727277 · Door Warning System
  > CAUTION 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)
- [SDR EISA98204](https://openairdocs.org/sdr/EISA98204.md): Skin · cracked · Aug 1, 1998 · N275WC · Boeing 727277 · Fuselage Main, Plate/Skin
  > DURING 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 HEAV
- [SDR EISA98184](https://openairdocs.org/sdr/EISA98184.md): Stringer · cracked · Aug 1, 1998 · N275WC · Boeing 727277 · Fuselage Main, Longeron/Stringer
  > DURING 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 53-10-0
- [SDR EISA98183](https://openairdocs.org/sdr/EISA98183.md): Connector · loose · Jul 27, 1998 · N275WC · Boeing 727277 · Pressure Regulator/Outflow Valve
  > RETURNED 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)
- [SDR EISA98066](https://openairdocs.org/sdr/EISA98066.md): Vhf Com · intermittent · Mar 23, 1998 · N275WC · Boeing 727277 · VHF Communications System
  > AFTER 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)
- [SDR EISA97227](https://openairdocs.org/sdr/EISA97227.md): Connector · loose · Nov 23, 1997 · N275WC · Boeing 727277 · Airspeed/Mach Indicator
  > ON 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)
- [SDR EISA97142](https://openairdocs.org/sdr/EISA97142.md): Fire Loop · inoperative · Jun 17, 1997 · N275WC · Boeing 727277 · Fire Detection
  > NR 3 FIRE WARNING WOULD NOT TEST. REMOVED AND REPLACED FIRE LOOP, REPAIRED WIRING TO CONNECTOR. (M)
- [SDR EISA95289](https://openairdocs.org/sdr/EISA95289.md): Connector · damaged · Sep 18, 1995 · N275WC · Boeing 727277 · Landing Gear Selector
  > GEAR 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)
- [SDR EISA95288](https://openairdocs.org/sdr/EISA95288.md): Skin · delamination · Sep 14, 1995 · N275WC · Boeing 727277 · Trailing Edge Flaps
  > LEFT INBOARD FORE FLAP LEADING EDGE SKIN DELAMINATED. REPAIRED FLAP PER SRM 57-50-4 AND SRM 51-60-6. (M)

Next page: https://openairdocs.org/deregistered/N275WC-2017-03-06/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N275WC-2017-03-06/reports

---
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