# Service difficulty reports: N612AW, cancelled Jan 31, 2008

A list on [N612AW, cancelled Jan 31, 2008](https://openairdocs.org/deregistered/N612AW-2008-01-31.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 · 82 reports

- [SDR A6WA200460054](https://openairdocs.org/sdr/A6WA200460054.md): Oxygen Mask · missing · Nov 10, 2004 · N612AW · Bag BAE146300A · Passenger Oxygen System
  > ROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IAW 35-20-45.
- [SDR A6WA200460033](https://openairdocs.org/sdr/A6WA200460033.md): Line · ruptured · Aug 31, 2004 · N612AW · Bac 146300A · Hydraulic System, Main
  > FOUND RIGHT MLG FAILED TO RETRACT AFTER TAKEOFF, REV UNSAFE LIGHT ILLUMINATED, CYCLED MLG DOWN, RETUREND TO RDU FOR FERRY FLIGHT BACK TO ATW. INSPECTED AND FOUND RT MLG FLEX LINE FOR RETRACTOR BRAKES RUPTURED WITH HYDRAULIC FUSE BLOWN, REPLACED LINE. RESET H
- [SDR A6WA200460023](https://openairdocs.org/sdr/A6WA200460023.md): Skin · damaged · Jun 14, 2004 · N612AW · Bac 146300A · Wing, Plate/Skin
  > FOUND LEFT INBOARD LEADING EDGE HAS WEAR DAMAGE OT THE INBOARD LEADING EDGE WHERE THE STALL BAR ATTACHES. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 612-190-006. (M)
- [SDR A6WA200460024](https://openairdocs.org/sdr/A6WA200460024.md): Skin · gouged · Jun 14, 2004 · N612AW · Bac 146300A · Horizontal Stabilizer, Plate/Skin
  > FOUND RIGHT HORIZONTAL STABILIZER TOP SKIN SMALL GOUGE IN THE UPPER SKIN OF THE RIGHT HORIZONTAL STABILIZER BETWEEN RIBS 9 AND 10. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 612-1909007. (M)
- [SDR A6WA200360027](https://openairdocs.org/sdr/A6WA200360027.md): Panel · chafed · May 12, 2003 · N612AW · Bac 146300A · Horizontal Stabilizer, Plate/Skin
  > CHAFE DAMAGE TO LEFT STABILIZER PANEL 275CL. MAINTENANCE BLENDED AND POLISHED DAMAGE AREA IAW BAE FAX BARA/AVR/3037/03-DC. (M)
- [SDR A6WA200260043](https://openairdocs.org/sdr/A6WA200260043.md): Tab · dented · Oct 8, 2002 · N612AW · Bac 146300A · Elevator, Tab Structure
  > DENTS TO RT ELEVATOR AND TABS X 34 RECEIVED CONCESSION.
- [SDR A6WA200260042](https://openairdocs.org/sdr/A6WA200260042.md): Tab · dented · Oct 8, 2002 · N612AW · Bac 146300A · Elevator, Tab Structure
  > DENTS TO LEFT ELEVATOR AND TABS X 8 RECEIVED CONCESSION.
- [SDR A6WA200260041](https://openairdocs.org/sdr/A6WA200260041.md): Structure · dented · Oct 8, 2002 · N612AW · Bac 146300A · Trailing Edge Flaps
  > RIGHT FLAP INBOARD AND OUTBOARD TABS DENTED, RECEIVED CONCESSION.
- [SDR A6WA200260040](https://openairdocs.org/sdr/A6WA200260040.md): Skin · dented · Oct 4, 2002 · N612AW · Bac 146300A · Fuselage Main, Plate/Skin
  > DENTS RIGHT FUSELAGE X 4 RECEIVED CONCESSION.
- [SDR A6WA200260039](https://openairdocs.org/sdr/A6WA200260039.md): Door · dented · Oct 4, 2002 · N612AW · Bac 146300A · Landing Gear Doors
  > DENTS RT MAIN LANDING GEAR X 26 RECEIVED CONCESSION.
- [SDR A6WA200260038](https://openairdocs.org/sdr/A6WA200260038.md): Door · dented · Oct 4, 2002 · N612AW · Bac 146300A · Landing Gear Doors
  > DENTS LEFT MAIN LANDING GEAR DOOR X 18 RECEIVED CONCESSION.
- [SDR A6WA200260037](https://openairdocs.org/sdr/A6WA200260037.md): Tab · dented · Oct 4, 2002 · N612AW · Bac 146300A · Leading Edge Devices
  > DENT LEFT FLAP INBOARD TAB X RECEIVED CONCESSION.
- [SDR A6WA200260036](https://openairdocs.org/sdr/A6WA200260036.md): Tab · dented · Oct 4, 2002 · N612AW · Bac 146300A · Ailerons
  > DENTS RIGHT AILERON INBOARD AND OUTBOARD TABS X 32 RECEIVED CONCESSION.
- [SDR A6WA200260035](https://openairdocs.org/sdr/A6WA200260035.md): Tab · dented · Oct 4, 2002 · N612AW · Bac 146300A · Ailerons
  > DENTS LEFT AILERON TABS X 9 RECEIVED CONCESSION.
- [SDR A6WA200100047](https://openairdocs.org/sdr/A6WA200100047.md): Control Box · failed · Aug 10, 2001 · N612AW · Bac 146300A · Turbine Governor
  > NR 1 ENGINE FAILED IN FLIGHT, NO LEAKS NOTED OR DAMAGE NOTED. MAINTENANCE REMOVED AND REPLACED THE HIGH AND LOW PRESSURE FUEL FILTERS, FUEL CONTROL AND PRIMARY OVERSPEED CONTROL BOX.
- [SDR A6WA200100039](https://openairdocs.org/sdr/A6WA200100039.md): O-Ring · failed · Jun 18, 2001 · N612AW · Bac 146300A · Hydraulic System, Main
  > LOST ALL GREEN HYDRAULIC QUANTITY ON GEAR EXTENSION. MAINTENANCE REMOVED AND REPLACED O-RING ON PTU PLUG.
- [SDR A6WA200100016](https://openairdocs.org/sdr/A6WA200100016.md): A/C Pack · failed · Feb 22, 2001 · N612AW · Bag BAE146300A · Cabin Cooling System
  > AT 20,000 FEET NR 1 PACK VALVE LIGHT CAME ON, FLIGHT CREW TRIED TO RESET COULD NOT. THE RECIRCULATION VALVE WENT FREST COULD NOT RESET. NR 2 PACK VALVE LIGHT CAME ON, LOST PRESSURE. RESTORED CABIN PRESSURE AT 10,000 FEET PACK WORKED. MAINTENANCE PRESSURIZE
- [SDR A6WA200000064](https://openairdocs.org/sdr/A6WA200000064.md): Service difficulty · Nov 7, 2000 · N612AW · Bag BAE146300A · APU Bleed Air System
  > STRONG OIL SMELL IN CABIN WHEN APU AIR INTRODUCED INTO SYSTEM OK ON ENGINE AIR. MAINTENANCE PERFORMED CONTAMINATED DUCT CLEANING PROCEDURE. APU VACUUM TEST GOOD.
- [SDR A6WA0000011](https://openairdocs.org/sdr/A6WA0000011.md): Engine · failed · Jan 31, 2000 · N612AW · Bag BAE146300A · Engine (Turbine/Turboprop)
  > FLT 5510 - ORD-ATW - NR 1 ENGINE FAILED ON TAKEOFF OUT OF ORD. REMOVED AND REPLACED NR 1 ENGINE. (M)
- [SDR 99ZZZM426](https://openairdocs.org/sdr/99ZZZM426.md): Skin · worn · Jun 29, 1998 · N612AW · Bag BAE146300A · Engine Cowling System
  > NR 2 ENGINE LEFT AFT AFT COWL DOOR INNER SKIN WORN THROUGH. PATCHED ABOVE DAMAGE PER PSI USING TA2 AND CHERRYMAXNUETS.
- [SDR 99ZZZM432](https://openairdocs.org/sdr/99ZZZM432.md): Door · lack of lube · Jun 24, 1998 · N612AW · Bag BAE146300A · Fixed Inner Doors
  > COCKPIT DOOR DIFFICULT TO OPEN FROM CABIN SIDE. LUBED AND RESHIMMED DOOR, OPS CHECK OK. (M)
- [SDR 99ZZZM544](https://openairdocs.org/sdr/99ZZZM544.md): Control Cable · corroded · Jun 19, 1998 · N612AW · Bag BAE146300A · Aileron Control System
  > LEFT MAIN AILERON CONTROL CABLES ARE CORRODED AT PULLEY BETWEEN FUSELAGE FRAME NR 24 AND 25. REMOVED AND REPLACED LEFT MAIN AILERON CENTER CONTROL CABLES, TENSIONED AND SAFETIED. (M)
- [SDR 99ZZZM427](https://openairdocs.org/sdr/99ZZZM427.md): Valve · failed · Jun 19, 1998 · N612AW · Bag BAE146300A · Passenger Oxygen System
  > CABIN OXYGEN MASKS AT RIGHT SIDE ROW 2 DEF VALVE PISTON FAIL TEST. REMOVED AND REPLACED VALVE AT SEAT 2 DEF, OPS CHECK GOOD. (M)
- [SDR 98ZZZM937](https://openairdocs.org/sdr/98ZZZM937.md): String · misinstalled · Jun 19, 1998 · N612AW · Bag BAE146300A · Passenger Oxygen System
  > OXYGEN CABIN DROP DOORS FOR MASKS AT POS RIGHT 7 DEF, RT 8 DEF, RT 12 DEF AND LT 5 ABC STRING HINGES ARE NOT LONG ENOUGH FOR DOOR TO SWING OPEN FULLY. ADJUSTED AND CHANGED STRINGS AT RT SIDE 7 DEF, 8 DEF, 12 DEF AND LT 5 ABC. ALL DOORS SWING FREE. OK FOR SE
- [SDR 98ZZZM908](https://openairdocs.org/sdr/98ZZZM908.md): Laynard · worn · Jun 19, 1998 · N612AW · Bag BAE146300A · Passenger Oxygen System
  > OXYGEN MASK AT 20 RT REBREATHER FEL HAS HOLES AND PIN STRING FRAYED, 11 LT. REBREATHER FELT HAS HOLES. REPLACED FELTS RT 20, 11 LT. REPLACED LANYARD 20 RT. CHECKS OK. (M)
- [SDR 99ZZZM547](https://openairdocs.org/sdr/99ZZZM547.md): Strip · cracked · Jun 18, 1998 · N612AW · Bag BAE146300A · Engine Cowling System
  > NR 4 ENGINE FORWARD OUTBOARD COWL DOORIS CRACKED AT INNER DOOR MIDDLE CAPPING. STRIP NEAR DRAIN LINE CLAMP. REPAIRED CAPPING STRIP PER BAE SRM 51-71-11 AND 12. (M)
- [SDR 99ZZZM546](https://openairdocs.org/sdr/99ZZZM546.md): Door · cracked · Jun 18, 1998 · N612AW · Bag BAE146300A · Engine Cowling System
  > NR 4 ENGINE INBOARD FAN DOOR, 3RD DOOR RIB, CRACKED AT LOWER CORNER AREA NEAR VENT TUBE. REPAIRED CRACK BY PATCHING IAW BAE AIR/WISC SRM STD PRACTICES AND FOUND SERVICABLE. (M)
- [SDR 99ZZZM545](https://openairdocs.org/sdr/99ZZZM545.md): Door · cracked · Jun 18, 1998 · N612AW · Bag BAE146300A · Engine Cowling System
  > NR 4 ENGINE INBOARD FAN DOOR, FORWARD INNER TITANIUM FIRESHIELD CRACKED AT CORNERS. REPAIRED CRACK BY PATCHING IAW BAE/AIR WISC SRM STD PRACTICES AND FOUND SERVICEABLE. (M)
- [SDR 99ZZZM537](https://openairdocs.org/sdr/99ZZZM537.md): Stiffener · cracked · Jun 15, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > RIGHT WING TE SHROUD LOWER SKIN STIFFENER CRACKED INBOARD OF RIB 10. REMOVED AND REPLACED LOWER SKIN STIFFENER PER SRM. (M)
- [SDR 98ZZZX3992](https://openairdocs.org/sdr/98ZZZX3992.md): Angle · missing · Jun 15, 1998 · N612AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > ATW - FORWARD CARGO BAY: CENTER FORWARD CARGO FLOOR SUPPORT ANGLE AT FRAME 19D, SECTION MISSING. REPLACED FORWARD CARGO BAY CENTER FLOOR SUPPORT ANGLE AT FRAME 19D.
- [SDR 98ZZZX3954](https://openairdocs.org/sdr/98ZZZX3954.md): Rib · cracked · Jun 15, 1998 · N612AW · Bag BAE146300A · Rudder, Spar/Rib
  > ATW - NR 1 (BOTTOM) RIB ON RUDDER IS CRACKED WITH A SMALL PIECE BROKEN OUT. REPLACED RIB PER REPAIR INSTRUCTIONS HC554H9005.
- [SDR 98ZZZX3956](https://openairdocs.org/sdr/98ZZZX3956.md): Skin · damaged · Jun 12, 1998 · N612AW · Bag BAE146300A · Fuselage Main, Plate/Skin
  > ATW - RIGHT MLG DOOR FORWARD LOWER CORNER DAMAGE DUE REPAIR IN 2,000 FLIGHTS PER AVRO FAX JM/0642-97. SEE SRM FOR SKIN REPAIR CRITERIA CURRENT TCA 25066 DUE REPAIR BY 27566 TCA. SEE FAX JM/RJ0317-98 FOR 500 FLIGHT EXTENSION TO 27566 TCA. REPAIRED FORWARD LO
- [SDR 99ZZZM543](https://openairdocs.org/sdr/99ZZZM543.md): Stiffener · cracked · Jun 11, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > LT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB NR 10. REPLACED LEFT TE WING SHROUD TOP SKIN STIFFENER INBOARD OF NR 10 RIB AT THIS TIME. (M)
- [SDR 99ZZZM542](https://openairdocs.org/sdr/99ZZZM542.md): Stiffener · cracked · Jun 11, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > LT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, OUTBOARD OF RIB NR 8. REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER OUTBOARD OF RIB NR 8.
- [SDR 99ZZZM540](https://openairdocs.org/sdr/99ZZZM540.md): Stiffener · cracked · Jun 11, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > LEFT WING TE SHROUD LOWER SKIN STIFFENERS, TWO HAVE TAG ANGLE CRACKED AT AFT END, BETWEEN RIBS 8/9. REPLACED TWO ANGLES ON TE SHROUD LOWER SKIN STIFFENERS BETWEEN RIBS 8/9 AT THIS TIME.
- [SDR 99ZZZM538](https://openairdocs.org/sdr/99ZZZM538.md): Stiffener · cracked · Jun 11, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > LEFT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB NR 6. REPLACED TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 JUST INBOARD OF RIB 6 AT THIS TIME. (M)
- [SDR 99ZZZM433](https://openairdocs.org/sdr/99ZZZM433.md): Angle · cracked · Jun 11, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > RIGHT WING TE TOP SKIN STIFFENER AFT TAG ANGLE CRACKED AT LOWER FLANGE BETWEEN RIBS 5 AND 6 OF SHROUD. REMOVED AND REPLACED AFT TAG ANGLE BETWEEN RIBS 5/6 FOR THE TOP SKIN STIFFENER. (M)
- [SDR 99ZZZM541](https://openairdocs.org/sdr/99ZZZM541.md): Stiffener · cracked · Jun 10, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > LT WING TE SHROUD TOP SKIN STIFFENER CRACK AT FORWARD END (BETWEEN RIBS 7/8). REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER BETWEEN RIB 7/8 AT THIS TIME.
- [SDR 99ZZZM435](https://openairdocs.org/sdr/99ZZZM435.md): Stiffener · cracked · Jun 8, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 OF SHROUD. REMOVED AND REPLACED STIFFENER PER SRM. (M)
- [SDR 99ZZZM434](https://openairdocs.org/sdr/99ZZZM434.md): Stiffener · cracked · Jun 8, 1998 · N612AW · Bag BAE146300A · Wing Miscellaneous Structure
  > RIGHT WING TOP SKIN TE STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB 9, SHROUD AREA. REMOVED AND REPLACED STIFFENER PER SRM. (M)
- [SDR 98ZZZX3957](https://openairdocs.org/sdr/98ZZZX3957.md): Skin · dented · Jun 8, 1998 · N612AW · Bag BAE146300A · Fuselage Main, Plate/Skin
  > ATW - REF W/C DATED 10-19-96, LT AFT FUSELAGE HAS DENT LOCATED 24 INCHES AFT OF LT PRESSURE BULKHEAD AND 6 INCHES BELOW 'N' NUMBERS. DENT IS 5 INCHES LONG BY MIN/D MAX - 1 INCHES/.078 INCH. REPAIRED DENT IAW BAE FAX DJR/RJO437-98.
- [SDR 99ZZZM539](https://openairdocs.org/sdr/99ZZZM539.md): Bracket · cracked · Jun 5, 1998 · N612AW · Bag BAE146300A · Hydraulic System, Main
  > LEFT WING TE, HYDRAULIC LINE CLAMP BRACKET CRACKED AT FALSE SPAR RIB NR 5. REPLACED HYDRAULIC LINE CLAMP BLOCK BRACKET AT RIB 5 AT THIS TIME. (M)
- [SDR 99ZZZM431](https://openairdocs.org/sdr/99ZZZM431.md): Control Cable · corroded · Jun 5, 1998 · N612AW · Bag BAE146300A · Aileron Control System
  > THE CENTER FUSELAGE INTERCONNECT CABLES ARE CORRODED AT RIGHT WING ROOT. REMOVED AND REPLACED BOTH CENTER FUSELAGE INTERCONNECT CABLES AND ADJUSTED IAW MM 27-11-00. W/CS GENERATED FOR FUNCTIONAL TEST OF AILERON CONTROLS AND DISCONNECT. (M)
- [SDR 99ZZZM430](https://openairdocs.org/sdr/99ZZZM430.md): Fitting · leaking · Jun 5, 1998 · N612AW · Bag BAE146300A · Crew Oxygen System
  > COCKPIT OXYGEN SYSTEM HAS A LEAK. FAILED LEAK CHECK. REMOVED AND REPLACED 'T' FITTING BETWEEN SUPPLY GAUGE AND PRESSURE REDUCING VALVE UNDER RIGHT SIDE PANEL. COMPLIED WITH LEAK CHECK. ALL IAW MM. (M)
- [SDR 99ZZZM429](https://openairdocs.org/sdr/99ZZZM429.md): Sill · corroded · Jun 5, 1998 · N612AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > FORWARD VESTIBULE, PAX AND SERVICE DOOR, SILL PLATE HAV SOME CORROSION AROUND SCREW HOLES AND OTHER SMALL AREAS. MINOR SURFACE CORROSION REMOVED FROM SILL PLATES, ALODINED AND PRIMED. (M)
- [SDR 99ZZZM428](https://openairdocs.org/sdr/99ZZZM428.md): Intercostal · corroded · Jun 5, 1998 · N612AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > GUSSET PLATE AND FORWARD REST FLOOR SUPPORT INTERCOSTAL, LEFT OF CENTER, AT FRAME 18 IS CORRODED. INSTALLED NEW GUSSET PLATE.
- [SDR 98ZZZX3958](https://openairdocs.org/sdr/98ZZZX3958.md): Cage · dented · Jun 5, 1998 · N612AW · Bag BAE146300A · Cargo/Baggage Doors
  > ATW - FORWARD CARGO DOOR AFT LOWER SEAL CAGE IS DENTED AND CRACKED. REPLACED FORWARD CARGO DOOR AFT LOWER SEAL CAGE.
- [SDR 98ZZZM868](https://openairdocs.org/sdr/98ZZZM868.md): Manifold · leaking · Jun 3, 1998 · N612AW · Bag BAE146300A · APU Engine Fuel and Control
  > NR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29.
- [SDR 98ZZZM867](https://openairdocs.org/sdr/98ZZZM867.md): Manifold · leaking · Jun 3, 1998 · N612AW · Bag BAE146300A · APU Engine Fuel and Control
  > NR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29.
- [SDR 98ZZZX3991](https://openairdocs.org/sdr/98ZZZX3991.md): Intercostal · corroded · Jun 2, 1998 · N612AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > ATW - AFT VESTIBULE FLOOR SUPPORT STRUCTURE, FIRST INTERCOSTAL INBOARD OF AIRSTAIR RAILS, LT SIDE HAS A RIVET WITH CORROSION AROUND IT. DRILLED OUT RIVET, REMOVED MINOR SURFACE CORROSION, USED PROTECTIVE TREATMENT ON BARE SURFACE, PRINTED AND COVERED SURFACE

Next page: https://openairdocs.org/deregistered/N612AW-2008-01-31/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 = 'N612AW' AND deregistration_id = 'N612AW-2008-01-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N612AW-2008-01-31/reports

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