# Service difficulty reports: N609AW, cancelled Dec 13, 2012

A list on [N609AW, cancelled Dec 13, 2012](https://openairdocs.org/deregistered/N609AW-2012-12-13.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 · 70 reports

- [SDR A6WA200560002](https://openairdocs.org/sdr/A6WA200560002.md): Brake · inoperative · Jan 11, 2005 · N609AW · Bac 146200A · Landing Gear Brake System
  > GREEN HYDRAULIC SYSTEM LOW, YELLOW SYSTEM HIGH. ABORTED TAKE-OFF AT LESS THAN 5 KTS. MAINTENANCE SERVICED AS REQUIRED. MAINTENANCE REMOVED AND REPLACED NR 4 BRAKE ASSEMBLY. (K)
- [SDR A6WA200360006](https://openairdocs.org/sdr/A6WA200360006.md): Lever · out of rig · Apr 11, 2003 · N609AW · Bac 146200A · Power Lever
  > NR 3 THRUST LEVER NEEDS TO BE RE-RIGGED. UNABLE TO SET BELOW 40 PERCENT N1. (M)
- [SDR A6WA200260002](https://openairdocs.org/sdr/A6WA200260002.md): Connector · failed · Feb 5, 2002 · N609AW · Bac 146200A · AC Generation System
  > ENROUTE, NR 1 GENERATOR FAILED, NO VOLTS OR HZ, NR 1 AC BUSS AND AC ESSENTIAL BUSS FELL OFF LINE. NR 4 GEN FELL OFF LINE MOMENTARILY WITH AC NR 2 BUSS OFF LINE ALSO. RESET NR 4 GENERATOR BUT ONLY ABLE TO REGAIN AC NR 2 BUSS. STARTED APU, APU GENERATOR SHOW
- [SDR A6WA200100021](https://openairdocs.org/sdr/A6WA200100021.md): Warning Light · illuminated · Mar 15, 2001 · N609AW · Bag BAE146200A · Leading Edge Slat Position Indicating System
  > FAULT LIGHT ILLUMINATED FLAPS STUCK AT 18 DEGREES. MAINTENANCE CLEARED FAULT USING BAE SUPPLEMENT. RAN FLAPS, OPS CHECKED GOOD.
- [SDR A6WA200000074](https://openairdocs.org/sdr/A6WA200000074.md): Connector · dirty · Dec 18, 2000 · N609AW · Bag BAE146200A · Landing Gear Brake System
  > DURING TAXI BRAKES SEEM INAFFECTIVE ON YELLOW HYDRAULIC SYSTEM. SWITCHED TO GREEN SYSTEM AND BACK TO YELLOW SYSTEM BRAKING NORMAL. MAINTENANCE REMOVED THE ANTI-SKID CONTROL BOX AND CLEANED CONNECTION OPERATIONAL CHECK GOOD. VISUALLY OBSERVED BRAKES ON YELLOW A
- [SDR A6WA200000068](https://openairdocs.org/sdr/A6WA200000068.md): Scoop · cracked · Nov 17, 2000 · N609AW · Bag BAE146200A · Engine Air Intake System
  > NR 1 ENGINE OUT BOARD DOOR NACA SCOOP AND ATTACHMENTS CRACKED. MAINTENANCE REPAIRED FAN DOOR NACA SCOOP AS REQUIRED ALSO REPAIRED APLITTER ANGLE IAW SRM AND FAX BARA/AVR/5228/00.
- [SDR A6WA200000067](https://openairdocs.org/sdr/A6WA200000067.md): Pin · cracked · Nov 11, 2000 · N609AW · Bag BAE146200A · Nose/Tail Landing Gear Attach Section
  > WHILE PERFORMING INSPECTION OF NLG RETRACTION BOSS FOUND EVIDENCE OF VISUAL FRETTING OF ATTACH PIN. FURTHER INSPECTION REVEALED TORQUE AT 20 FT LBS AND SIGNS OF CRACKING VISUALLY CONFIRMED BY NDT SIDEWALL BAD. MAINTENANCE REPLACED NOSE DIAPHAGM PER RIL HC53H9
- [SDR A6WA9900039](https://openairdocs.org/sdr/A6WA9900039.md): Girt Bar · disengaged · Apr 18, 1999 · N609AW · Bag BAE146200A · Emergency Equipment
  > AFT PASSENGER CABIN DOOR AFTER OPENING, GIRT BAR DISENGAGED FROM DOOR. FOUND NO PARTIAL DEPLOYMENT OF SLIDE, RE-ENGAGED GIRT BAR TO DOOR. RECONNECTED SLIDE AUTODEPLOY LANYARD. OPS CHECKED DOOR AND GIRT BAR. OPS CHECKS SATISFACTORY. ACFT TT: 23,562 HOUR
- [SDR 98ZZZX3959](https://openairdocs.org/sdr/98ZZZX3959.md): Actuator · leaking · Oct 4, 1998 · N609AW · Bag BAE146200A · Entrance Stairs
  > ATW - FLT 581 - YELLOW HYDRAULIC FLUID LOST, WITH ASSOCIATED FLUID AT REAR AIRSTAIR AND LAVATORY. FOUND AFT AIRSTAIR, FORWARD ACTUATOR LEAKING, CLEANED, CAPPED OFF LINE AND DEFERRED AND PLACARDED, C/W OVERWEIGHT LANDING INSPECTION.
- [SDR 99ZZZM493](https://openairdocs.org/sdr/99ZZZM493.md): Skin · chafed · Jun 24, 1998 · N609AW · Bag BAE146200A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CHAFED APPROX 13 INCHES LONB BY FORWARD RIGHT WING ROOT FAIRING BETWEEN FRAMES 25/26. REF W/C 6075 FOR BLEND AND NDT. FIT EXTERNAL PATCH OVER CHAFED AREA UNDER RT WING ROOT FAIRING ON FUSELAGE SKIN BETWEEN FRAMES 25/26 PER SRM 53-00-12 FIGURE 2
- [SDR 99ZZZM534](https://openairdocs.org/sdr/99ZZZM534.md): Prox Switch · failed · May 12, 1998 · N609AW · Bag BAE146200A · Landing Gear Position and Warning
  > WITH GEAR HANDLE SELECTOR UP, LEFT MAIN GEAR INDICATES GEAR INTRANSIT, RID LIGHT IN GEAR HANDLE ALSO ILLUMINATED. NO AURAL GEAR WEARING. STANDBY GEAR INDICATORS ALL OFF. REMOVED AND REPLACED LEFT MLG LEG UPLOCK HARNESS AND PROXIMITY SWITCH IAW BAE 146MM, TE
- [SDR 99ZZZM561](https://openairdocs.org/sdr/99ZZZM561.md): Arm · failed · Mar 30, 1998 · N609AW · Bag BAE146200A · Landing Gear Retraction/Extension System
  > DURING GEAR RETRACTION AT EGE, HEARD A VERY LOUD BANG FROM NOSE WHEEL AREA ACCOMPANIED BY WHEEL ROTATION SOUNDS. GEAR RETRACTION AND EXTENSION NORMAL. REPLACED LEFT EMEREGNCY LOWERING GEAR ASSISTING ARM ASSY. RETRACTED GEAR, FREE FALL OPS CHECKED GOOD. CLO
- [SDR 99ZZZM500](https://openairdocs.org/sdr/99ZZZM500.md): Bolts · loose · Mar 26, 1998 · N609AW · Bag BAE146200A · Wing Miscellaneous Structure
  > FOUND LOOSE JOBOLTS AT VARIOUS LOCATIONS AT WING TANK RIB '0' AND RIB 2 LT/RT. COMPLETED LOOSE JOBOLT REPLACEMENT AT RIB 0 AND RIB 2 LT/RT PER RIL HC571H9033. NOTE, 6 POSITIONS WERE OVERSIZED.
- [SDR 99ZZZM563](https://openairdocs.org/sdr/99ZZZM563.md): Stall Bar · loose · Mar 25, 1998 · N609AW · Bag BAE146200A · Stall Warning System
  > LEFT WING INBOARD SECTION OF STALL BAR LOOSE, PULLING OVER SCREW HEADS. REMOVED LT WING STALL TRIGGER AND REPAIRED PER FAX REF DJH/RJO268-98 USING FAX GCB/RJ1344-94. REINSTALLED STALL TRIGGER. (M)
- [SDR 99ZZZM492](https://openairdocs.org/sdr/99ZZZM492.md): Stall Bar · out of position · Mar 25, 1998 · N609AW · Bag BAE146200A · Stall Warning System
  > RIGHT WING SHORT SECTION OF STALL BAR PULLING OVER CORNER SCREWS. REMOVED LEFT WING STALL TRIGGER AND REPAIR PER FAX REF DJH/R JO268 USING FAX GCB/RJ1344-94 AND REINSTALLED STALL TRIGGER. (M)
- [SDR 99ZZZM511](https://openairdocs.org/sdr/99ZZZM511.md): Wire · broken · Mar 24, 1998 · N609AW · Bag BAE146200A · Fire Detection
  > NR 1 ENGINE POWER LEVER FIRE WARNING LIGHT DOES NOT ILLUMINATE DURING FIRE TEST, WIRE BAD. REMOVED AND REPLACED BOTH WIRES IN POWER LEVER FIRE WARNING. TESTED PER MM. (M)
- [SDR 99ZZZM507](https://openairdocs.org/sdr/99ZZZM507.md): Bulkhead Strip · corroded · Mar 24, 1998 · N609AW · Bag BAE146200A · Fuselage Main, Bulkhead
  > FORWARD LAVATORY BULKHEAD I2109 LOWER METAL STRIP ON BOTTOM OF BULKHEAD IS CORRODED. INSTALLED LOWER METAL STRIP ON FORWARD LAVATORY BULKHEAD I2109 OLD UNIT PREVIOUSLY REMOVED. (M)
- [SDR 99ZZZM564](https://openairdocs.org/sdr/99ZZZM564.md): Stiffener · cracked · Mar 19, 1998 · N609AW · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING TE TOP SKIN, TWO STIFFENERS CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0626-0000). REPAIRED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0627-002)
- [SDR 99ZZZM562](https://openairdocs.org/sdr/99ZZZM562.md): Angle · cracked · Mar 19, 1998 · N609AW · Bag BAE146200A · Passenger/Crew Doors
  > LEFT FORWARD PAX DOOR HANDLE BOX AREA 2 CRACKED ANGLES. REPLACED LEFT FORWARD PAX DOOR HANDLE BOX AREA ANGLES REF P/N'S ABOVE. REPAIR ACCOMPLISHED IAW BAE DRAWINGS HC521H0508 AND HC521H0507 AND BAE FAX REF DJR/RJO318-97. (M)
- [SDR 99ZZZM502](https://openairdocs.org/sdr/99ZZZM502.md): Bolt · worn · Mar 19, 1998 · N609AW · Bag BAE146200A · Spoilers
  > RIGHT AIRBRAKE UPPER ATTACH POINT BOLT PLATING IS WORN OFF, BOLT WAS FROZEN IN BEARING. REMOVED AND REPLACED HINGE PIN AND BUSH. INSTALLED DURING AIRBRAKE INSTALLATION. SEE W/C NR 3019 FOR INSTALLATION. (M)
- [SDR 99ZZZM567](https://openairdocs.org/sdr/99ZZZM567.md): Stiffener · cracked · Mar 18, 1998 · N609AW · Bag BAE146200A · Wing Miscellaneous Structure
  > RIGHT WING TE TOP SKIN STIFFENER CRACKED AT AFT END BETWEEN RIBS 3/4. REMOVED AND REPLACED STIFFENER. (M)
- [SDR 99ZZZM498](https://openairdocs.org/sdr/99ZZZM498.md): Skin · chafed · Mar 17, 1998 · N609AW · Bag BAE146200A · Landing Gear Doors
  > RIGHT MLG DOOR INTERNAL SKIN, FORWARD EDGE, APPROX 1ST 6 INCHES DOWN HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN L/G IS UP AND LOCKED. BLENDED OUT CHAF IN DRUM, MINOR DAMAGE WITHIN LIMITS, PRC COATED FOR ABRASION. (M)
- [SDR 99ZZZM491](https://openairdocs.org/sdr/99ZZZM491.md): Pulley · seized · Mar 17, 1998 · N609AW · Bag BAE146200A · Aileron Control System
  > RIGHT WING LOWER AILERON TRIM CABLE PULLEY SEIZED OUTBOARD OF NR 4 FLAP TRACK. REMOVED AND REPLACED TRIM CABLE PULLEY'S AS NEEDED IAW MM. (M)
- [SDR 99ZZZM490](https://openairdocs.org/sdr/99ZZZM490.md): Attach Links · corroded · Mar 17, 1998 · N609AW · Bag BAE146200A · Aerodynamic Fairings
  > RIGHT WING TO FUSELAGE AFT ATTACH LINKS HAVE SURFACE CORROSION ON ENDS (PAINT MISSING). CLEANED, PRIMED AND PAINTED ENDS. (M)
- [SDR 99ZZZM566](https://openairdocs.org/sdr/99ZZZM566.md): Bracket · cracked · Mar 16, 1998 · N609AW · Bag BAE146200A · Hydraulic System, Main
  > RIGHT WING TE HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR ABOVE NR 2 FLAP TRACK. REPLACED RIGHT WING TE HYD LINE CLAMP BRACKET. (M)
- [SDR 99ZZZM499](https://openairdocs.org/sdr/99ZZZM499.md): Bolts · loose · Mar 16, 1998 · N609AW · Bag BAE146200A · Wing Miscellaneous Structure
  > PERFORM RIL HC571H9033 LT RIB 2 OUTBOARD JOBOLTS. PERFORMED RIL HC571H9033 ON LEFT RIB 2 OUTBOARD JOBOLTS. (M)
- [SDR 99ZZZM568](https://openairdocs.org/sdr/99ZZZM568.md): Stiffener · cracked · Mar 14, 1998 · N609AW · Bag BAE146200A · Wing Miscellaneous Structure
  > RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN 7/8. (M)
- [SDR 99ZZZM487](https://openairdocs.org/sdr/99ZZZM487.md): Stiffener · cracked · Mar 14, 1998 · N609AW · Bag BAE146200A · Wing Miscellaneous Structure
  > RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 (OUTBOARD STIFFENER). REPLACED RT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 7/8. (M)
- [SDR 99ZZZM569](https://openairdocs.org/sdr/99ZZZM569.md): Skin · chafed · Mar 13, 1998 · N609AW · Bag BAE146200A · Trailing Edge Flaps
  > RIGHT FLAP UPPER SKIN BETWEEN RIB 29/30 HAS.020 INCH DEEP BY 1 INCH LONG CHAFE. BLENDED CHAFE MARK TO A SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO236-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO236-98, AREA CRACK FREE. APPLIED SURFACE REPROTECTION A
- [SDR 99ZZZM565](https://openairdocs.org/sdr/99ZZZM565.md): Skin · chafed · Mar 13, 1998 · N609AW · Bag BAE146200A · Trailing Edge Flaps
  > RIGHT FLAP TAB UPPER SKIN AT RIB 34 HAS TWO.011 INCH DEEP CHAFED AREAS, (.005 TO.008). BLENDED CHAFE MARKS TO SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO234-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO234-98, AREA CRACK FREE. APPLIED SURFACE REPROTE
- [SDR 99ZZZM497](https://openairdocs.org/sdr/99ZZZM497.md): Skin · chafed · Mar 13, 1998 · N609AW · Bag BAE146200A · Landing Gear Doors
  > LEFT MLG DOOR INTERNAL SKIN FORWARD EDGE APPROX 1ST 6 INCHES FROM TOP EDGE HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN GEAR IS UP AND LOCKED. TRANSFER TO W/O BX1879 FOR REPAIR. (M)
- [SDR 99ZZZM489](https://openairdocs.org/sdr/99ZZZM489.md): False Spar · cracked · Mar 13, 1998 · N609AW · Bag BAE146200A · Wing Miscellaneous Structure
  > RIGHT WING TE FALSE SPAR CRACKED JUST INBOARD OF INBOARD LIFT SPOILER JACK. REPAIRED PER FAX JM/RJ0240-98, PER DRAWING HC572H9036. OPPOSITE HAND TO DRAWING. (M)
- [SDR 99ZZZM501](https://openairdocs.org/sdr/99ZZZM501.md): Bolt · scratched · Mar 12, 1998 · N609AW · Bag BAE146200A · Rudder Actuator
  > UPPER RUDDER ACTUATOR AFT ATTACHMENT BOLT HAS SCRATCH THAT GOES BELOW PLATING. REMOVED AND REPLACED UPPER RUDDER ACTUATOR AFT ATTACHMENT BOLT IAW AMM. (M)
- [SDR 99ZZZM504](https://openairdocs.org/sdr/99ZZZM504.md): Bearing · worn · Mar 11, 1998 · N609AW · Bag BAE146200A · Rudder Structure
  > RUDDER TOP 'A FRAME HINGE POINT HAS A BAD BEARING. 'A' FRAME REMOVED FOR REPAIR. INSTALLED SERVICEABLE RUDDER TOP 'A' FRAME IAW BAE MM. (M)
- [SDR 99ZZZM494](https://openairdocs.org/sdr/99ZZZM494.md): Door · damaged · Mar 11, 1998 · N609AW · Bag BAE146200A · Landing Gear Doors
  > RIGHT MLG DOOR LOWER FORWARD CORNER IS DEFORMED OUTWARD APPROX.167 FROM CONTOUR, APPROX 3.55 IN LENGTH. REPAIRED IAW BAE SRM 52-81-11, FIG 204, TYPE 2. (M)
- [SDR 99ZZZM488](https://openairdocs.org/sdr/99ZZZM488.md): Mount · cracked · Mar 11, 1998 · N609AW · Bag BAE146200A · Spoilers
  > RIGHT WING ROOT, LIFT SPOILER CONTROL VALVE MOUNT PLATE CRACKED. REMOVED AND REPLACED PLATE. (M)
- [SDR 99ZZZM510](https://openairdocs.org/sdr/99ZZZM510.md): Control Cable · corroded · Mar 10, 1998 · N609AW · Bag BAE146200A · Aileron Control System
  > LEFT CLAD INTERCONNECT CABLE FOR AILERONS SHOWS EVIDENCE OF CORROSION AT DIFFERENTIAL SECTOR BETWEEN RIBS 14/15. REMOVED AND REPLACED LEFT CLAD INTERCONNECT CABLE (AILERON) IAW BAE MM. GENERATED W/C TO PERFORM AILERON FUNCTIONAL CHECKS AND PRIORITY 2 WC TO R
- [SDR 99ZZZM508](https://openairdocs.org/sdr/99ZZZM508.md): Control Cable · corroded · Mar 10, 1998 · N609AW · Bag BAE146200A · Aileron Control System
  > RIGHT WING AILERON INTERCONNECT CABLES AT WING ROOT PULLEY CORRODED. REMOVED AND REPLACED FUSELAGE INTERCONNECT CABLES (AILERON) IAW BAE MM. GENERATED WC TO PERFORM AILERON FUNCTIONAL CHECK AND PRI 2 WC TO RE-CHECK TENSION AT 4000 FLT INTERVAL. (M)
- [SDR 99ZZZM506](https://openairdocs.org/sdr/99ZZZM506.md): Cable Guard · seized · Mar 10, 1998 · N609AW · Bag BAE146200A · Aileron Control System
  > RIGHT WING ROOT, OUTBOARD CABLE GAURD SEIZED AND BOTH PULLEYS WORN FOR CENTER SECTION AILERON INTERCONNECT CABLES. REMOVED AND REPLACED PULLEYS EXTRACTED SEIZED GUARD AND REPLACED WITH NEW GUARD, RIGHT WING ROOT. (M)
- [SDR 99ZZZM570](https://openairdocs.org/sdr/99ZZZM570.md): Seal · bent · Mar 9, 1998 · N609AW · Bag BAE146200A · Cargo/Baggage Doors
  > FORWARD CARGO DOOR BOTTOM HALF SEAL CAGE IS DISTORTED, BENT IN NUMEROUS AREAS. REPLACED FORWARD CARGO DOOR BOTTOM AFT SEAL CAGE P/N HC523J0 063-202. STRAIGHTENED BEND IN PORTION OF BOTTOM FORWARD SEAL CAGE. (M)
- [SDR 99ZZZM496](https://openairdocs.org/sdr/99ZZZM496.md): Seal · damaged · Mar 9, 1998 · N609AW · Bag BAE146200A · Cargo/Baggage Doors
  > REAR CARGO DOOR LOWER SEAL CAGE IS BENT, DEFORMED IN SEVERAL AREAS. REPLACED REAR CARGO DOOR LOWER SEAL CAGE. (M)
- [SDR 99ZZZM505](https://openairdocs.org/sdr/99ZZZM505.md): Bearing · worn · Mar 5, 1998 · N609AW · Bag BAE146200A · Rudder Structure
  > RUDDER BEARING BAD AT MAIN (RIB 6) 'A' FRAME SUPPORT. ALLOW AND EXCESSIVE UP AND DOWN FLOAT OF RUDDER ASSY.25 INCH APPROX. REMOVED AND REPLACED RUDDER MAIN 'A' FRAME (RIB 6) HINGE BEARING. (M)
- [SDR 99ZZZM503](https://openairdocs.org/sdr/99ZZZM503.md): Control Cable · corroded · Mar 5, 1998 · N609AW · Bag BAE146200A · Elevator Control System
  > LEFT AND RIGHT ELEVATOR CABLES ARE CORRODED AT PULLEYS IN VERTICLE STAB. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR CABLES FROM REAR PRESS BULKHEAD TO COMPENSATORS AND ADJUSTED IAW MM 27-31-00. W/C GENERATED FOR FUNCTION TEST. (M)
- [SDR 99ZZZM509](https://openairdocs.org/sdr/99ZZZM509.md): Sill · cracked · Mar 4, 1998 · N609AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > AFT PASSENGER DOOR, AFT SIDE OF DOOR SILL PLATE IS CRACKED ABOUT 1 INCH LONG. REMOVED DAMAGED SILL PLATE, DRILLED AND FITTED NEW SILL PLATE ON AFT PASSENGER DOOR, AFT SIDE INSTALLED NEW SILL PLATE AND PAINTED RIVET HEADS AND BUCKTAILS. (M)
- [SDR 99ZZZM495](https://openairdocs.org/sdr/99ZZZM495.md): Bracket · cracked · Feb 27, 1998 · N609AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > UPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM HAS A CRACK. REPLACED UPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM. (M)
- [SDR 97ZZZX3147](https://openairdocs.org/sdr/97ZZZX3147.md): Air Distribution · fumes · Apr 20, 1997 · N609AW · Bag BAE146200A · Air Distribution System
  > ORD - FLT 504 - NOTICED FUMES IN CABIN ON GROUND WHILE ON APU AIR. RAN BOTH PACKS TO FULL HOT. NO FUMES NOTED.
- [SDR 97ZZZX2992](https://openairdocs.org/sdr/97ZZZX2992.md): Hydraulic Line · leaking · Apr 20, 1997 · N609AW · Bag BAE146200A · Hydraulic System, Main
  > ORD - FLT 504 - SUSPECT HYDRAULIC FLUID FUMES IN AIRCRAFT. FOUND LEAKING NLG DOWN LINE. REPLACED LINE, GREEN SYSTEM.
- [SDR 97ZZZM402](https://openairdocs.org/sdr/97ZZZM402.md): Doubler · cracked · Dec 5, 1996 · N609AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > RIGHT STIFFENER (STATION 47.20) AT FRAME 29 IN HYDRAULIC BAY HAS CRACKED DOUBLER PLATE AT BOTTOM END OF STIFFENER. REPLACED RIGHT STIFFENER (STATION 47.20) AT FRAME 29 IAW BAE DRAWING NR HC536H0090 AND AIR FAX NR DS/W/TS/25913/96.
- [SDR 97ZZZM403](https://openairdocs.org/sdr/97ZZZM403.md): Trim Chain · corroded · Dec 3, 1996 · N609AW · Bag BAE146200A · Aileron Control System
  > LEFT AILERON TRIM SCREWJACK CHAIN APPEARS TO BE CORRODED. LEFT TRIM CABLE TURNBUCKLES LOOSE. REMOVED AND REPLACED LEFT AILERON TRIM CHAIN IAW 27-12-17. A DJUSTED CABLES AND COMPLIED WITH FUNCTION TEST IAW 27-12-00. CHECKS OK. (M)
- [SDR 97ZZZM404](https://openairdocs.org/sdr/97ZZZM404.md): Floorbeam · cracked · Dec 2, 1996 · N609AW · Bag BAE146200A · Fuselage Main, Floor Beam
  > THREE FLOORBEAMS ARE CRACKED AT FRAME 29 BEAM 3, 13 AND 19. REPAIRED CRACKS IAW BAE DRAWING HC536H9211 AND FAX AIRAMS/T/BAE/25858/96.

Next page: https://openairdocs.org/deregistered/N609AW-2012-12-13/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 = 'N609AW' AND deregistration_id = 'N609AW-2012-12-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N609AW-2012-12-13/reports

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