# Service difficulty reports: N742RW, cancelled Jan 17, 2008

A list on [N742RW, cancelled Jan 17, 2008](https://openairdocs.org/deregistered/N742RW-2008-01-17.md).

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

- [SDR C7WA200600010](https://openairdocs.org/sdr/C7WA200600010.md): Coupling · broken · Apr 19, 2006 · N742RW · Boeing 7272M7 · Hydraulic System, Auxiliary
  > FLIGHT RETURN: LOSS OF ALL B-SYSTEM HYDRAULIC FLUID AND QUANTITY. REPLACED BROKEN HYDRAULIC QUICK DISCONNECT COUPLING TO NR1 B-SYSTEM HYDRAULIC PUMP. SYSTEM OPERATIONAL AND LEAK CHECKS GOOD IAW MM. (K)
- [SDR C7WA200500116](https://openairdocs.org/sdr/C7WA200500116.md): Indicator · inoperative · Aug 24, 2005 · N742RW · Boeing 7272M7 · Landing Gear Position and Warning
  > NOSE LANDING GEAR DOWN AND LOCKED INDICATOR LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. FOLLOWED ABNORMAL PROCEDURES, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE LANDING GEAR GREEN LIGHT ASSEMBLY PER MM 33-10-51. OPS CHECKS GOOD. (M)
- [SDR C7WA200500115](https://openairdocs.org/sdr/C7WA200500115.md): Wire · shorted · Aug 20, 2005 · N742RW · Boeing 7272M7 · Fire Protection System Wiring
  > AIR TURNBACK, NR 3 ENGINE FIRE DETECTOR INOPERATIVE LIGHT ILLUMINATED AND NR 3 ENGINE FIRE WARNING LIGHT AND BELL WENT OFF REPEATEDLY 7 TIMES. FOUND NR 3 ENGINE B-LOOP WIRE SHORTED. REPAIRED WIRE PER B727 MM 20-00-00. OPS CHECKS GOOD PER 26-11-01. (M)
- [SDR C7WA0500109](https://openairdocs.org/sdr/C7WA0500109.md): Line · loose · Jul 12, 2005 · N742RW · Boeing 7272M7 · Turbine Engine Oil System
  > AIR TURNBACK: ENGINE SHUTDOWN, NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON AT 8000 FT, DURING CLIMB OUT. COMPLETED PRECAUTIONARY SHUTDOWN CHECKLIST. DURING INSPECTION OF NR 1 ENGINE, FOUND LOOSE LINE B-NUT AT OIL PRESSURE SWITCH. TIGHTENED B-NUT. OPERATIO
- [SDR C7WA200500109](https://openairdocs.org/sdr/C7WA200500109.md): Connector · loose · Jul 12, 2005 · N742RW · Boeing 7272M7 · Turbine Engine Oil System
  > AIR TURNBACK; ENGINE SHUTDOWN, NR 2 EGT FLUCTUATES AT FLIGHT LEVEL 27,000. OIL PRESSURE DROPPED TO ZERO, OIL QUANTITY FOLLOWED TO ZERO. DURING INSPECTION OF NR 2 ENGINE FOUND INLET CASE TUBE CONNECTOR ASSEMBLY LOOSE AND LEAKING. TIGHTENED LOOSE BOLTS. LEA
- [SDR C7WA200300078](https://openairdocs.org/sdr/C7WA200300078.md): Wire · shorted · Jan 13, 2005 · N742RW · Boeing 7272M7 · Air Conditioning System Wiring
  > NR 1 PACK VALVE CIRCUIT BREAKER POPPED ON CLIMB-OUT, CIRCUIT BREAKER WOULD NOT RESET. TROUBLESHOOTING PERFORMED BY WD 21-61-02, FOUND WIRE SHORTED. ACCOMPLISHED REPAIR BY WIRE SPLICE, AIR COND SYSTEM. TESTED WITH BOTH PACKS ON TESTED GOOD. (M)
- [SDR C7WA200300051](https://openairdocs.org/sdr/C7WA200300051.md): Connector · loose · Dec 19, 2003 · N742RW · Boeing 7272M7 · Electrical Connectors
  > FLIGHT RETURN, AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT. CLEANED AND RESEATED CONNECTOR AT LOWER AFT BODY OVERHEAT SENSING ELEMENT, OPS CHECK NORMAL IAW MM 20-60-01 AND 26-14-0. (M)
- [SDR C7WA200300043](https://openairdocs.org/sdr/C7WA200300043.md): Tube · broken · Apr 24, 2003 · N742RW · Boeing 7272M7 · Engine Bleed Air System
  > AIR TURNBACK, ENGINE NR 3 HAD MULTIPLE COMPRESSOR STALLS. FOUND BROKEN LINE AT PRESSURE BLEED CONTROL VALVE REMOVED AND REPLACED TUBE IAW MM 20-10-05 ACCOMPLISHED ENGNE RUN IAW MM 71-00-00, ALL PARAMTERS NORMAL. (M)
- [SDR EISA20010118](https://openairdocs.org/sdr/EISA20010118.md): Wire · loose · Aug 29, 2001 · N742RW · Boeing 7272M7 · Door System Wiring
  > TAKEOFF DISCONTINUED AT 100 KTS DUE TO MAIN CARGO DOOR LIGHT ON STEADY, RETURNED TO RAMP, LIGHT REMAINS ON.CORRECTIVE ACTION:TROUBLESHOT MAIN CARGO DOOR IAW AERO. M/M, FOUND WIRING FROM SWITCH PULLED LOOSE. REPAIRED WIRING. OPS CK OK.
- [SDR EISA20010091](https://openairdocs.org/sdr/EISA20010091.md): Skin · cracked · May 4, 2001 · N742RW · Boeing 7272M7 · Passenger/Crew Doors
  > L-1 LOWER DOOR HINGE AT FUSELAGE SKIN CRACKED. REPAIRED CRACK, ROUTING OUT AND FABRICATING AND INSTALLING REPAIR FILLER AND DOUBLER IAW 727 SB 727-53-0198 REV 1 FIGURE 4 DATED 07-25-1991.
- [SDR EISA20000206](https://openairdocs.org/sdr/EISA20000206.md): Skin · cracked · Nov 6, 2000 · N742RW · Boeing 7272M7 · Fuselage Main, Plate/Skin
  > 10 INCH CRACK, 1 INCH HOLE, AND 8 INCH CREASE FORWARD OF C1 DOOR. CORRECTIVE ACTION: FABRICATED DOUBLER, FILLERS, AND SHIMS, ALODINED, PRIMED, AND INSTALLED IAW 53-30-3 FIG 6, 51-10-2, 53-10-3 FIG 1 AND FIG 2, 53-10-4 FIG 13, 51-30-2, M/M 34-11-0052-35-21 AN
- [SDR EISA2000044](https://openairdocs.org/sdr/EISA2000044.md): Switch · out of adj · Apr 8, 2000 · N742RW · Boeing 7272M7 · Leading Edge Slat Control System
  > LEFT LEADING EDGE NUMBER THREE FLAP LIGHT ILLUMINATED IN TURBULENT CONDITIONS. ADJUSTED POSTION INDICATOR MICROSWITCH ON NR 3 LEADING EDGE FLAP. OPERATIONAL CHECK GOOD. (M)
- [SDR EISA99170](https://openairdocs.org/sdr/EISA99170.md): Moisture Trap · full · Sep 22, 1999 · N742RW · Boeing 7272M7 · Engine Drains
  > NR 3 ENGINE EPR AND FUEL FLOW FLUCTUATING. ABORTED TAKEOFF. INSPECTED ENGINE AND DRAINED WATER TRAP. NO DEFECT NOTED PER 727 MM CHAPTER 73-00. (M)
- [SDR EISA99014](https://openairdocs.org/sdr/EISA99014.md): Nav Control · shorted · Jan 27, 1999 · N742RW · Boeing 7272M7 · Integrated Flight System
  > CAPTAIN CDI OSCILLATES ONE DOT LEFT AND RIGHT ON LOC/VOR FREQUENCY, CAPTAIN RMI PIVOTS 10 DEGREES LEFT AND RIGHT ON VOR/LOC FREQUENCY. BOTH OCCUR ALSO WHEN CAPTAIN ON AUX. REMOVED AND REPLACED GPS NMC AND NAV CONTROL HEAD OPS CHECK GOOD ON GROUND. TEST FLIG
- [SDR 99ZZZM350](https://openairdocs.org/sdr/99ZZZM350.md): Nmc · shorted · Jan 27, 1999 · N742RW · Boeing 7272M7 · Integrated Flight System
  > CAPTAIN CDI OSCILLATES ONE DOT LEFT AND RIGHT ON LOC/VOR FREQUENCY, CAPTAIN RMI PIVOTS 10 DEGREES LEFT AND RIGHT ON VOR/LOC FREQUENCY. BOTH OCCUR ALSO WHEN CAPTAIN ON AUX. REMOVED AND REPLACED GPS NMC AND NAV CONTROL HEAD OPS CHECK GOOD ON GROUND. TEST FLIG
- [SDR EISA98246](https://openairdocs.org/sdr/EISA98246.md): Light · inoperative · Oct 4, 1998 · N742RW · Boeing 7272M7 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE OVER MAIN ENTRY DOOR. GENERATED FROM MAINTENANCE REPORT. REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD IAW MM CHAPTER 33. (M)
- [SDR EISA98056](https://openairdocs.org/sdr/EISA98056.md): Wire · broken · Mar 19, 1998 · N742RW · Boeing 7272M7 · Landing Gear System Wiring
  > ON TAKEOFF IN MSP, THE GEAR FAILED TO RETRACT, PERFORMED CHECKLIST AND RETRACTED GEAR BY PULLING THE OVERRIDE RELEASE LATCH, FLIGHT CONTINUED TO FINAL DESTINATION CANCUN. TROUBLESHOT ELECTRICAL CIRCUIT. ONE BROKEN WIRE WAS FOUND IN SOLENOID CONNECTOR. REPAI
- [SDR EISA97153](https://openairdocs.org/sdr/EISA97153.md): Detector · failed · Jun 25, 1997 · N742RW · Boeing 7272M7 · Air Distribution System
  > AFTER TAKEOFF "NO RACK COOLING' LIGHT ON AT 9000 FEET MSL AND OFF DURING DESCENT ALT 2000 FT MSL. REMOVED AND REPLACED FLOW LIMITING NOZZLE DUCT AND COOLING EFFECT DETECTOR OPS CHECKED OK PER MM 21-58-31. (M)
- [SDR EISA97141](https://openairdocs.org/sdr/EISA97141.md): Light · loose · Jun 17, 1997 · N742RW · Boeing 7272M7 · Emergency Lighting
  > EMERGENCY FLOOR STRIP LIGHTING BUCKLING AT ROW 18. RESECURED FLOOR TRACK LIGHTING AT ROW 18. (X)
- [SDR EISA97100](https://openairdocs.org/sdr/EISA97100.md): Light · loose · May 20, 1997 · N742RW · Boeing 7272M7 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING IS LOOSE ON RIGHT SIDE ROW 17. RESECURED TRACK. OPS PER MM 33-50-0. (X)
- [SDR EISA97098](https://openairdocs.org/sdr/EISA97098.md): Outflow Valve · dirty · May 16, 1997 · N742RW · Boeing 7272M7 · Pressure Regulator/Outflow Valve
  > AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION. CABIN CLIMBED AT 1500 FPM. CARGO HEAT OUTFLOW CLOSED, CABIN CLIMBED AT 500 FPM, AIR TURN BACK. ALL DOOR SEALS AND DUCTS CHECKED GOOD. NO LEAKS IN PRESSURIZATION CHECKS, CLEANED OUTFLOW VALVE AND FUNCTIONALLY CHEC
- [SDR EISA97087](https://openairdocs.org/sdr/EISA97087.md): Lamp · failed · May 5, 1997 · N742RW · Boeing 7272M7 · Emergency Lighting
  > FORWARD EXIT LIGHTS NOT ILLUMINATED. RELAMPED FORWARD EXIT SIGN. OPS CHECK IS GOOD. (M)
- [SDR EISA97088](https://openairdocs.org/sdr/EISA97088.md): Skin · lightning strike · May 3, 1997 · N742RW · Boeing 7272M7 · Elevator, Plate/Skin
  > DURING C-CHECK, FOUND LIGHTNING STRIKE OUTBOARD LEFT ELEVATOR UPPER TRAILING EDGE. INSTALLED REPAIR PER SRM 55-20-1. (M)
- [SDR EISA97094](https://openairdocs.org/sdr/EISA97094.md): Skin · gouged · May 2, 1997 · N742RW · Boeing 7272M7 · Wing, Plate/Skin
  > DURING C-CHECK, FOUDN LEFT UPPER WING LEADING EDGE, WS 510 HAS DEEP GOUGES AND ELONGATED HOLES AFT OF NR 3 SLAT. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-4. (M)
- [SDR EISA97093](https://openairdocs.org/sdr/EISA97093.md): Elevator · cracked · May 2, 1997 · N742RW · Boeing 7272M7 · Elevator, Plate/Skin
  > DURNG C-CHECK, FUOND X-RAY INSPECTION OF LEFT ELEVATOR REVEALS A 3 INCH CRACK AT INBOARD END OF ELEVATOR AS SHOWN IN SHOT NR 1. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-1 AND 51-30-02. (M)
- [SDR EISA97092](https://openairdocs.org/sdr/EISA97092.md): Fitting · corroded · May 2, 1997 · N742RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND LEFT WING INBOARD FORE FLAP APPROX 1 SQUARE INCH IN AREA AND.1875 INCH DEPTH OF CORROSION, OUTBOARD END 4 INCHES ABOVE TE. REMOVED AND REPLACED FLAP END FITTING PER MM 27-51-32. (M)
- [SDR EISA97091](https://openairdocs.org/sdr/EISA97091.md): Fitting · cracked · May 2, 1997 · N742RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND LEFT WING OUTBOARD TRAILING EDGE FORE FLAP ATTACH FITTING AT INBOARD CARRIAGE IS CRACKED. REPLACED ATTACH FITTING PER MM 27-51-01. (M)
- [SDR EISA97090](https://openairdocs.org/sdr/EISA97090.md): Intercostal · torn · May 2, 1997 · N742RW · Boeing 7272M7 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FORWARD CARGO PIT FS 577 STRINGER 23L INTERCOSTAL HAS.25 INCH TEAR AT FORWARD CUTOUT. REPAIRED INSTALLED PER SRM 51-10-1. (M)
- [SDR EISA97089](https://openairdocs.org/sdr/EISA97089.md): Skin · torn · May 2, 1997 · N742RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND NR 3 LE SLAT TRAILING EDGE UPPER SKIN IS TORN IN TWO PLACES. REPAIRED SKIN PER SRM 57-50-02 AND 51-30-02. (M)
- [SDR 9608282771](https://openairdocs.org/sdr/9608282771.md): Power Supply · inoperative · Apr 14, 1996 · N742RW · Boeing 7272M7 · Emergency Lighting
  > DURING PREFLIGHT, FOUND EXTERIOR EMERGENCY LIGHT AT DOOR 2L AND 2R INOPERATIVE. REPLACED POWER SUPPLIES AND BATTERIES, CHECKED.
- [SDR 9601532771](https://openairdocs.org/sdr/9601532771.md): Power Supply · inoperative · Jan 23, 1996 · N742RW · Boeing 7272M7 · Emergency Lighting
  > DURING PREFLIGHT, FOUND SECTION OF FLOOR PATH EMERGENCY LIGHTS LEFT SIDE OF CABIN INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, CHECKED OK.
- [SDR 9601512771](https://openairdocs.org/sdr/9601512771.md): Mix Valve · failed · Jan 21, 1996 · N742RW · Boeing 7272M7 · Cabin Cooling System
  > DURING FLIGHT, LOSE RIGHT AIR CONDITIONING PACK WITH LOSS OF PRESSURIZATION. AIRCRAFT DROPPED TO 10,000 FEET AND RETURNED TO MSP. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT HAND PACK MIX VALVE AND OPERATIONAL CHECK OK.
- [SDR 9515122771](https://openairdocs.org/sdr/9515122771.md): Torque Link · disconnected · Oct 5, 1995 · N742RW · Boeing 7272M7 · Nose/Tail Landing Gear
  > DURING LANDING ROLLOUT, SEVERE VIBRATION FROM NOSE WHEEL AND STEERING BECAME INOPERATIVE. AIRCRAFT WAS TOWED TO GATE. MAINTENANCE FOUND NOSE GEAR TORQUE LINK DISCONNECTED AND GROUND SHIFT ARM BENT. REPLACED UPPER TORQUE LINK AND OPERATIONAL CHECK NORMAL.
- [SDR 9511812771](https://openairdocs.org/sdr/9511812771.md): Controller · malfunctioned · Aug 3, 1995 · N742RW · Boeing 7272M7 · Cabin Pressure Controller
  > AFTER LEVEL OFF AT FL 240 WITH SINGLE PACK OPERATION, LEFT CABIN ALTITUDE CONTINUED A 200 FPM CLIMB. UNABLE TO CONTROL BY ALTERNATE MEANS. FLIGHT JETTISONED 10,000 LBS OF FUEL, DIVERTED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED AUTO P
- [SDR 9505862771](https://openairdocs.org/sdr/9505862771.md): Frame · cracked · Apr 13, 1995 · N742RW · Boeing 7272M7 · Emergency Exits
  > DURING PERIODIC CHECK, MAINTENANCE FOUND RIGHT FORWARD EMERGENCY EXIT OUTSIDE HANDLE OPENING FRAME CRACKED. DEFERRED CASTING REPLACEDMENT PER MAINTENANCE MANUAL 52-21-00. NWA IS REPLACING MAGNESIUM CASTINGS WITH AN ALUMINUM PART DUE TO MULTIPLE FINDINGS.
- [SDR 9505852771](https://openairdocs.org/sdr/9505852771.md): Frame · cracked · Apr 13, 1995 · N742RW · Boeing 7272M7 · Emergency Exits
  > DURING PERIODIC CHECK, MAINTENANCE FOUND RIGHT AFT EMERGENCY EXIT OUTSIDE HANDLE OPENING FRAME CRACKED. DEFERRED CASTING REPLACEMENT PER MAINTENANCE MANUAL 52-21-00. NWA IS REPLACING MAGNESIUM CASTINGS WITH AN ALUMINUM PART DUE TO MULTIPLE FINDINGS.
- [SDR 9505432771](https://openairdocs.org/sdr/9505432771.md): Seat Track · corroded · Apr 4, 1995 · N742RW · Boeing 7272M7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PERIODIC CHECK, MAINTENANCE FOUND SEAT TRACK AT FS 383, RBL 24 CORRODED ON OUTBOARD SIDE. REPAIRED PER SRM 53-10-5 FIG 9 AND NWA EA 27-96518.

## 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 = 'N742RW' AND deregistration_id = 'N742RW-2008-01-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N742RW-2008-01-17/reports

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