# Service difficulty reports: N606AW, cancelled Nov 15, 2011

A list on [N606AW, cancelled Nov 15, 2011](https://openairdocs.org/deregistered/N606AW-2011-11-15.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 · 76 reports

- [SDR A6WA200460055](https://openairdocs.org/sdr/A6WA200460055.md): Acm · malfunctioned · Nov 11, 2004 · N606AW · Bag BAE146200A · Cabin Cooling System
  > NR PACK TEMP IS UNCONTROLLABLE IN EITHER MANUAL OR AUTO WHEN USING APU AIR. WILL RUN FULL HOT AND SMOKES CABIN. NOTE: CONTROLLABLE IN (MAN) MODE WITH ENGINE AIR, OTHERWISE SMOKES CABIN. PACK NR 2 HIGH TEMP LIGHT COMES ON. MAINTENANCE REMOVED AND REPLACED N
- [SDR A6WA200460021](https://openairdocs.org/sdr/A6WA200460021.md): Warning Light · illuminated · Jun 7, 2004 · N606AW · Bac 146200A · Landing Gear Position and Warning
  > AFTER GEAR UP SELECTED LEFT MLG RED INDICATION STAYED ILLUMINATED WITH GEAR INTRANSIT IN GEAR HANDLE ILLUMINATED GEAR SELECTED DOWN ALL NORMAL INDICATIONS. MAINTENANCE FOUND LEFT GEAR DOOR IN THE OPEN FOR MAINTENANCE POSITION. CLOSED DOOR FOR FLIGHT. (M)
- [SDR A6WA200360041](https://openairdocs.org/sdr/A6WA200360041.md): Bracket · improper · Sep 29, 2003 · N606AW · Bac 146200A · Elevator Miscellaneous Structure
  > LEFT ELEVATOR NR 2 HINGE 'A' FRAME TOP MOUNTING BOLT HAS AN IMPROPER SAFETY BRACKET, POORLY MANUFACTURED. REPLACED WITH NWE PART NR HC551B0098-000. (M)
- [SDR A6WA200360040](https://openairdocs.org/sdr/A6WA200360040.md): Skin · damaged · Sep 27, 2003 · N606AW · Bac 146200A · Trailing Edge Flaps
  > DAMAGED RIGHT OUTBOARD FLAP TAB BOTTOM SKIN BETWEEN RIBS 21-22. REPAIR IAW BAE FAX BARA/AVR/6530/03-DC. (M)
- [SDR A6WA200360043](https://openairdocs.org/sdr/A6WA200360043.md): Stringer · corroded · Sep 24, 2003 · N606AW · Bac 146200A · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 33 RIGHT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101 AVMAX NON-ROUTINE 2289 FOR REPAIR. REPAIRED STRINGER IAW BAE SRM 53-00-12 FIG 207. (M)
- [SDR A6WA200360042](https://openairdocs.org/sdr/A6WA200360042.md): Stringer · corroded · Sep 24, 2003 · N606AW · Bac 146200A · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 33 LEFT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101. REV AVMAX NON-ROUTINE 1204 FOR REPAIR. REPAIRED STRINGER IAW SRM 53-00-12 FIG 207. (M)
- [SDR A6WA200360038](https://openairdocs.org/sdr/A6WA200360038.md): Structure · damaged · Sep 10, 2003 · N606AW · Bac 146200A · Trailing Edge Flaps
  > DAMAGED BUSHING BORES AT LT WING FLAP STRUCTURE AT TRACK 2. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060005. (M)
- [SDR A6WA200360037](https://openairdocs.org/sdr/A6WA200360037.md): Door Frame · gouged · Sep 8, 2003 · N606AW · Bac 146200A · Fuselage Main, Structure
  > AFT CARGO DOOR OUTSIDE DOOR SURROUND GOUGED AT TOP AFT RADIUS MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060004. (M)
- [SDR A6WA200360034](https://openairdocs.org/sdr/A6WA200360034.md): Skin · damaged · Sep 6, 2003 · N606AW · Bac 146200A · Cargo/Baggage Doors
  > DAMAGE EXTERNAL SKIN TO THE FORWARD CARGO DOOR MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060001. (M)
- [SDR A6WA200360035](https://openairdocs.org/sdr/A6WA200360035.md): Structure · cracked · Sep 6, 2003 · N606AW · Bac 146200A · Fuselage Main, Structure
  > FOUND CRACK AT RIVET LOCATION JUST AFT OF FRAME 29 STRINGER 13 LT. MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060002. (M)
- [SDR A6WA200360036](https://openairdocs.org/sdr/A6WA200360036.md): Frame · corroded · Sep 6, 2003 · N606AW · Bac 146200A · Fuselage Main, Frame
  > FOUND CORROSION ON FRAME 18 MAINTENANCE REQUESTED REPAIR FROM BAE REF AVMAX FAX NR 1655-6060003. (M)
- [SDR A6WA200360028](https://openairdocs.org/sdr/A6WA200360028.md): A/C Pack · smoke · May 13, 2003 · N606AW · Bac 146200A · Cabin Cooling System
  > PACKS EMITTING SMOKE INTO CABIN MAINTENANCE REMOVED AND REPLACED APU, PERFORMED PACK BURNOUT IAW AWAC SUPP 96.31. (M)
- [SDR A6WA200260034](https://openairdocs.org/sdr/A6WA200260034.md): Clamp · out of position · Aug 20, 2002 · N606AW · Bac 146200A · Landing Gear Actuator
  > DAMAGE TO THE MAIN LANDING GEAR BAY SKIN AT FRAME 29 LEFT SIDE AS CAUSED BY DOWN LOCK ACTUATOR CLAMP. MAINTENANCE DAMAGE BLENDED OUT IAW SRM 51-10-2. (M)
- [SDR A6WA200100008](https://openairdocs.org/sdr/A6WA200100008.md): Web · damaged · Jan 30, 2001 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > DAMAGE TO WEBS ABOVE AND BELOW FORWARD PASSENGER DOOR DAMPER CAN. MAINTENANCE REMOVED AND REPLACED DAMPER CAN LOWER AND UPPER WED ASSEMBLIES IAW BAE 146 SRM.
- [SDR A6WA200100007](https://openairdocs.org/sdr/A6WA200100007.md): Longeron · cracked · Dec 21, 2000 · N606AW · Bag BAE146200A · Fuselage Main, Longeron/Stringer
  > LONGERON ON THE RT SIDE, AT THE TOP OF SERVICE DOOR AFT OF FRAME 19 AT THE FRAME HAS A CRACK. MAINTENANCE FOUND CLEAT OF DIAPHRAM CRACKED AND REPAIRED BY PATCHING IAW BAE SRM 51-71-11 AND FOUND SERVICEABLE.
- [SDR A6WA200100006](https://openairdocs.org/sdr/A6WA200100006.md): Frame · cracked · Dec 15, 2000 · N606AW · Bag BAE146200A · Fuselage Main, Frame
  > FOUND SEVERE CORROSION AND CRACKING ON THE AFT SIDE OF FRAME 18, ON THE I/B FRAME FLANGE 8 INCHES ABOVE FLOOR LEVEL AND 4 INCHES TO 8 INCHES BELOW FLOOR LEVEL. MAINTENANCE C/W PARTIAL FRAME REPLACEMENT OF FRAME 18 LT IAW RIL HC537H9453 & BAE FAX REF BARA/AVR/
- [SDR A6WA9900128](https://openairdocs.org/sdr/A6WA9900128.md): Brake · failed · Dec 1, 1999 · N606AW · Bag BAE146200A · Landing Gear Brake System
  > FLT 5545 - ORD-MLI - AFTER CHOCKS WERE PULLED. AIRCRAFT STARTED ROLLING FORWARD, BRAKING DID NOT STOP AIRCRAFT. AIRCRAFT HIT TERMINAL BLDG. AIRCRAFT REMOVED FROM SERVICE FOR REPAIR. (M)
- [SDR 99ZZZM607](https://openairdocs.org/sdr/99ZZZM607.md): Stringer · dented · Nov 3, 1998 · N606AW · Bag BAE146200A · Fuselage Main, Longeron/Stringer
  > HAT STRINGER ON AFT WALL OF APU BOX IS DENTED. REPLACED HAT STRINGER ON AFT APU FIREWALL IAW BAE FAXES BARA/AVR/1885/98 AND DWC/RJ0002-98. (M)
- [SDR 99ZZZM606](https://openairdocs.org/sdr/99ZZZM606.md): Cables · corroded · Nov 3, 1998 · N606AW · Bag BAE146200A · Elevator Control System
  > LEFT AND RIGHT MAIN ELEVATOR CONTROL CABLES ARE CORRODED AT VERTICAL STABILIZER REAR SPAR PULLEYS. REMOVED AND REPLACED ALL FOUR MAIN ELEVATOR CONTROL CABLES FROM REAR PRESS BULKHEAD TO CABLE COMPENSATORS, ADJUSTED IAW MM. W/C GENERATED FOR FUNCTION ALL TEST
- [SDR 99ZZZM604](https://openairdocs.org/sdr/99ZZZM604.md): Floorbeam · cracked · Nov 2, 1998 · N606AW · Bag BAE146200A · Fuselage Main, Floor Beam
  > FOUND CRACK IN FLOORBEAM AT FRAME NR 37 UNDER FLOOR PANEL 241DF IN CENTER ON FWD SIDE OF BEAM ABOUT 8 INCHES LONG AND 1 INCH FROM TOP OF BEAM. REMOVED CRACKED AREA OF FRAME 37 AND REPAIRED IAW BAE DRAWING NR HC538H9219 AND BAE FAX REF RJO778-98 DATED 11/2/98.
- [SDR 99ZZZM610](https://openairdocs.org/sdr/99ZZZM610.md): Diaphragm · cracked · Oct 28, 1998 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > NLG ACTUATOR AT UPPER ATTACHMENT POINT DIAPHRAGM IS CRACKED IN THE WEB AND BOSS. REPORTED TO BAE RDO. REF W/C 7025 FOR CORRECTIVE ACTION, DIAPHRAGM REPLACEMENT.
- [SDR 99ZZZM609](https://openairdocs.org/sdr/99ZZZM609.md): Diaphragm · cracked · Oct 27, 1998 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > NOSE SIDEWALL DIAPHRAGM REMOVED FOR CRACKED ACTUATOR ATTACH POINT. REPLACED NLG LEFT DIAPHRAGM PER BAE FAX REF NR JEN/RJO0505-98. GEN W/C FOR 60 CYC DV INSPECTIONS AND 2000 AND OR 10 MONTH REPLACEMENT. (M)
- [SDR 99ZZZM608](https://openairdocs.org/sdr/99ZZZM608.md): Control Cable · corroded · Oct 16, 1998 · N606AW · Bag BAE146200A · Elevator Tab Control System
  > ELEVATOR TRIM CABLE BETWEEN SCREWJACKS HAS SIGNS OF CORRISON AT CENTER PULLEY. ALSO, CENTER PULLEY BEARING WORN. REMOVED AND REPLACED CENTER PULLEY AND TRIM CABLE BETWEEN SCREWJACKS. ADJUSTED TENSION IAW MM 27-32-00. REF W/C 3055 FOR FUNCTIONAL TEST. (M)
- [SDR 99ZZZM602](https://openairdocs.org/sdr/99ZZZM602.md): Engine · failed · Sep 22, 1998 · N606AW · Bag BAE146200A · Engine (Turbine/Turboprop)
  > NR 1 EGINE FAILE AND FIRE IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM ANS AWAC GMM ENG CHANGE CHECKLIST VOLUME II SEC B CHAP 72, COMPLIED WITH ALL REQ'D ENGINE GROUND RUNS. ALL PARAMETERS FOUND SATISFACTORY. (M)
- [SDR 98ZZZM928](https://openairdocs.org/sdr/98ZZZM928.md): Engine · failed · Sep 22, 1998 · N606AW · Bag BAE146200A · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FAIL/SAFE AND FIRE INFLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM AND AWAC GMM ENGINE CHANGE CHECKLIST VOLUME II SEC B CHAP 72. COMPLIED WITH ALL REQUIRED ENGINE GROUND RUNS. ALL PARAMETERS FOUND SATISFACTORY. (M)
- [SDR 98ZZZM927](https://openairdocs.org/sdr/98ZZZM927.md): Poppet Valve · failed · Mar 28, 1998 · N606AW · Bag BAE146200A · Engine Anti-Icing System
  > NR 4 ENGINE READS 7 PERCENT BELOW N1 REF AT 904 DEGREES TGT, ABORTED TAKEOFF AT LESS THAN 60 KTS, RETURNED TO GATE AT DEN. REPLACED FCU POPPET VALVE ASY. ENGINE STILL LOW ON POWER. (M)
- [SDR 98ZZZX1187](https://openairdocs.org/sdr/98ZZZX1187.md): Generator · failed · Nov 11, 1997 · N606AW · Bag BAE146200A · AC Generator-Alternator
  > DEN - FLT 587 - APU GENERATOR WENT OFF-LINE AND WOULD NOT RESET. FAILURE ACCOMPANIED BY ELECTRICAL SMELL WHEN APU AIR IS USED. INSPECTED APU, OIL LEVELS OK. INSPECTED MAG PLUG AND FILTERS, NO CONTAMINATION NOTED. STARTED APU, APU GEN OPS NORMALLY UNDER LOA
- [SDR 97ZZZX2990](https://openairdocs.org/sdr/97ZZZX2990.md): Spoiler Light · illuminated · May 26, 1997 · N606AW · Bag BAE146200A · Drag Control System
  > DEN - FLT 655 - AFTER TAKEOFF GEAR RETRACTED, SPOILER LOCK-UP LIGHT ILLUMINATED ALONG WITH MAIN SPOILER FAULT LIGHT. RETURNED FOR LANDING. UPON GEAR DOWN, MAIN SPOILER FAULT LIGHT EXTINGUISHED, LEFT SPOILER GLARESHIELD LIGHTS ILLUMINATED. C/W FAULT ISO CHAR
- [SDR 97ZZZX2991](https://openairdocs.org/sdr/97ZZZX2991.md): Slide · damaged · May 21, 1997 · N606AW · Bag BAE146200A · Escape Slide
  > LEFT FORWARD EVACUATION SLIDE PACK-BOARD STRUCTURE WAS TORN AND SLIDE PARTIALLY PULLED FROM DOOR. REPLACED SLIDE.
- [SDR 97ZZZM395](https://openairdocs.org/sdr/97ZZZM395.md): Relay · failed · Nov 21, 1996 · N606AW · Bag BAE146200A · Landing Gear Retraction/Extension System
  > UNABLE TO RAISE GEAR UNLESS OVERRIDE IS SELECTED. GEAR SELECTED DOWN NORMAL EXTENSION. REMOVED AND REPLACED RELAY GF4 SYSTEM CHECKS GOOD. (M)
- [SDR 97ZZZM396](https://openairdocs.org/sdr/97ZZZM396.md): Angle · cracked · Nov 10, 1996 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > MACHINED ANGLE ATTACHED TO SEAT RAIL 5 INCHES AFT OF FRAME 28 TO 6 INCHES AFT OF FRAME 29 LEFT OUTBOARD CRACKED. REPLACED ANGLE, REF FAX FOR HI-LOKS IN LIEU OF SP157 FAX NR DJR/RJ1282-96. (M)
- [SDR 97ZZZM463](https://openairdocs.org/sdr/97ZZZM463.md): Support · cracked · Nov 7, 1996 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT AT FRAME 20A CRACKED AT CENTER GUSSET PLATE. REPAIRED FRAME 20A FLOOR SUPPORT IAW AVRO FAX REF NR DJR/R J1269-96.
- [SDR 97ZZZM462](https://openairdocs.org/sdr/97ZZZM462.md): Skin · chafed · Nov 7, 1996 · N606AW · Bag BAE146200A · Trailing Edge Flaps
  > REF FAX JM/RJ0927-6 DATED 8/14/96, LT FLAP TAB UPPER SKIN CHAFES AT RIBS 19 AND 21, FORWARD OF THE SPOILER RIB STRIP. REQUIRE REPAIR BY 34682 TCA. AWAC FAX LM185-96 REFERS. REPAIRED IAW AVRO REPAIR DRAWING HC579H9080, HC579H9074 AND FAX REP NR JM/RJ1109-96.
- [SDR 97ZZZM464](https://openairdocs.org/sdr/97ZZZM464.md): Seat Rail · corroded · Nov 6, 1996 · N606AW · Bag BAE146200A · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD VESTIBULE FRAME 18 RIGHT INBOARD SEAT RAIL CORRODED IN SEVERAL SPOTS, REF SRM 53-00-32 PAGE 203 AND 51-31-11 PAGE 22. REPAIRED FORWARD VESTIBLE RT INBOARD SEAT RAIL BY SPLICING NEW RAIL IN PLACE PER SRM 53-00-32 PAGES 202, 203, 204. SPLICED PLACE WAS
- [SDR 97ZZZM466](https://openairdocs.org/sdr/97ZZZM466.md): Floorbeam · cracked · Nov 5, 1996 · N606AW · Bag BAE146200A · Fuselage Main, Floor Beam
  > CRACK INDICATIONS FOUND ON THREE PRESSURE FLOORBEAMS OVER FRAME NR 32 LEFT SIDE. VERIFIED WITH ET INSPECTION. REPAIRED 3 CRACKS AT FRAME 32 IAW AVRO REPAIR DRAWING HC536H9211 AND FAX REF NR DJR/RJ1228-96 AND DJR/RJ1209-96.
- [SDR 97ZZZM465](https://openairdocs.org/sdr/97ZZZM465.md): Floorbeam · cracked · Nov 5, 1996 · N606AW · Bag BAE146200A · Fuselage Main, Floor Beam
  > ELEVEN CRACK INDICATIONS ON FORWARD END OF PRESSURE FLOORBEAMS AT FRAME 29. CRACKED BEAMS ARE NR 2, 3, 4, 5, 6, 7, 9, 13, 15, 19 AND 20 NUMBERED L TO RT. REPAIRED 11 CRACKS AT FRAME 29 IAW AVRO REPAIR DRAWING HC536H9211 AND FAX REP NR DJR/RJ1228-96 AND DJR/R
- [SDR 97ZZZM454](https://openairdocs.org/sdr/97ZZZM454.md): Rib · chafed · Nov 1, 1996 · N606AW · Bag BAE146200A · Wing, Rib/Bulkhead
  > RIB ABOVE LEFT NR 1 FLAP TRACK IS CHAFED WHERE IT CONTACTS ACCESS PANEL 285FT. BLENDED AND REPROTECTED THE CHAFE MARK ON THE SIDE OF RIB 2 TRAILING EDGE EXTENSION PER FAX DJR/RJ1243-96 DATED OCT 31, 1996 AND SRM 51-20-11. GENERATED W/C TO C/W A DV INSPECTION
- [SDR 97ZZZM453](https://openairdocs.org/sdr/97ZZZM453.md): Flap Track · worn · Nov 1, 1996 · N606AW · Bag BAE146200A · Trailing Edge Flaps
  > NR 1 FLAP TRACK LEFT SIDE HAS.020 INCH WEAR ON SIDE OF LOWER AND UPPER RAILS, FROM SLIPPER PLATES. BLENDED THE OUTBOARD SIDE OF THE LEFT NR 1 FLAP TRACK UPPER AND LOWER RAILS PER FAX DJR/RJ1243-96, DATED OCT 31, 1996.
- [SDR 97ZZZM449](https://openairdocs.org/sdr/97ZZZM449.md): Bolts · too long · Oct 30, 1996 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > FUSELAGE BOLT LOOSE AT RIGHT WING FORWARD SPAR. CHECK TORQUE ON THREE OTHER IN THAT SAME ROW. REPLACED 2 BOLTS FOUND TO BE TOO LONG. CHECK TORQUE ON REMAINING 3, CHECK OK. WITCOBOND 2 REPLACEMENT BOLTS, HOLES WITHIN LIMITS. AFT OF FR 26 WING TO FUSELAGE C
- [SDR 97ZZZM452](https://openairdocs.org/sdr/97ZZZM452.md): Angles · broken · Oct 29, 1996 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AT FRAME NR 35, RT BELLY TIE DOWN AREA, SURROUND PLATE BENT AND ANGLES TO FRAME BROKEN. ALSO, MISSING RIVETS IN FRAME. STRAIGHTEN PLATE AND REPLACED ANGLE AND REPLACED RIVETS.
- [SDR 97ZZZM386](https://openairdocs.org/sdr/97ZZZM386.md): Cables · corroded · Oct 29, 1996 · N606AW · Bag BAE146200A · Aileron Control System
  > PERFORMED AILERON INTERCONNECT CABLE CHECK. FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED IAW AMM GENERATED W/C FOR FUNCTIONAL CHECK.
- [SDR 97ZZZM385](https://openairdocs.org/sdr/97ZZZM385.md): Cables · corroded · Oct 29, 1996 · N606AW · Bag BAE146200A · Aileron Control System
  > LEFT AND RIGHT AILERON INTERCONNECT CABLES COVER SLEEVES ARE WORN IN TWO AT CABLE GUIDES. REMOVED AND REPLACED LEFT AND RIGHT AILERON INTERCONNECT CABLES IAW AMM W/C GENERATED FOR FUNCTIONAL CHECKS. REF W/C 2365. (M)
- [SDR 97ZZZM384](https://openairdocs.org/sdr/97ZZZM384.md): Flap Tracks · worn · Oct 29, 1996 · N606AW · Bag BAE146200A · Trailing Edge Flaps
  > LEFT WING NR 2 FLAPTRACK WEARMARKS LOWER RAIL OUTBOARD EDGE FRM SLIP P/PLATE. WEARMARKS 94) BOTH SIDES TOP OF LOWER RAIL FROM ROLLERS AND 1, UPPER RAIL OUTBOARD EDGE FROM SIDE ROLL. COMPLIED WITH BLENDING OF WEARMARKS ON UPPER OUTBOARD RAIL AND BOTH SIDES ON
- [SDR 97ZZZM461](https://openairdocs.org/sdr/97ZZZM461.md): Rail · corroded · Oct 23, 1996 · N606AW · Bag BAE146200A · Passenger/Crew Doors
  > FORWARD VESTIBULE INBOARD AIRSTAIR RAIL NEEDS TO BE REPLACED DUE TO CORROSION. RAIL IS REMOVED. REPLACED FORWARD INBOARD AIRSTAIR RAIL.
- [SDR 97ZZZM459](https://openairdocs.org/sdr/97ZZZM459.md): Bolts · failed · Oct 23, 1996 · N606AW · Bag BAE146200A · Spoilers
  > LEFT WING INBOARD LIFT SPOILER JACK BOLTS, FORWARD AND AFT, FAILED NDT. INSTALLED NEW FORWARD AND AFT JACK BOLTS ON LEFT INBOARD LIFT SPOILER.
- [SDR 97ZZZM458](https://openairdocs.org/sdr/97ZZZM458.md): Blkhd Doubler · cracked · Oct 23, 1996 · N606AW · Bag BAE146200A · Fuselage Main, Bulkhead
  > IN HYD BAY AT FRAME 29 BULKHEAD, THE TWO MOST OUTBOARD STIFFENERS LEFT AND RIGHT WERE FOUND TO HAVE CRACKED DOUBLERS AT BOTTOM BOLT HOLE. THESE STIFFENERS ARE NOT COVERED IN EO E95/003/653, STATION 47.20 LT/RT, END OF CRACKS MARKED WITH GREASE PENCIL. REPLAC
- [SDR 97ZZZM457](https://openairdocs.org/sdr/97ZZZM457.md): Blkhd Stiffeners · cracked · Oct 23, 1996 · N606AW · Bag BAE146200A · Fuselage Main, Bulkhead
  > PERFORMED ET AT FRAME 29 BULKHEAD TO C/W EO E95/003/653 ITEM NR 3. FOUND CRACKS AT STIFFENER STATION 36.62, 31.13, 25.94 LEFT AND 36.62, 31.13, 25.94 RT. REPAIR STIFFENERS IAW EO E95/005/654. END OF CRACKS MARKED WITH GREASE PENCIL. REPAIRED FRAME 29 STIFF
- [SDR 97ZZZM456](https://openairdocs.org/sdr/97ZZZM456.md): Support · corroded · Oct 23, 1996 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > FRAME 20 LEFT SIDE FLOOR SUPPORT BEAM HAS CORROSION WHERE BOTH FORWARD AIRSTAIR RAILS ATTACH. NEEDS TO BE CLEANED AND MEASURED FOR DEPTH. REPAIR OR REPAINT AS NECESSARY (ONLY ONE SIGNIFICANT SPOT W/A DEPTH MAX AT.029 INCH). REPAIRED IAW FAX DJR/RJ1197-96.
- [SDR 97ZZZM377](https://openairdocs.org/sdr/97ZZZM377.md): Hi-Lok · sheared · Oct 22, 1996 · N606AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > SIGHTING ATTACHMENT ON (BELLY) LONGERON FITTING OF FRAME NR 29 HAS HI-LOK SHEARED. REPLACED BROKEN HI-LOK IAW BAE 146MM (SAME PART AS ORIGINAL). (M)
- [SDR 97ZZZM378](https://openairdocs.org/sdr/97ZZZM378.md): Rail · corroded · Oct 21, 1996 · N606AW · Bag BAE146200A · Passenger/Crew Doors
  > REAR AIRSTAIR, INBOARD RAIL CORRODED NEEDS TO BE REPLACED. REMOVED AND REPLACED AFT INBOARD AIRSTAIR RAIL. (M)

Next page: https://openairdocs.org/deregistered/N606AW-2011-11-15/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 = 'N606AW' AND deregistration_id = 'N606AW-2011-11-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N606AW-2011-11-15/reports

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