# Service difficulty reports: N607AW, cancelled Jul 20, 2006

A list on [N607AW, cancelled Jul 20, 2006](https://openairdocs.org/deregistered/N607AW-2006-07-20.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 · 72 reports

- [SDR A6WA200560021](https://openairdocs.org/sdr/A6WA200560021.md): Flap System · malfunctioned · Mar 6, 2006 · N607AW · Bag BAE146200A · Trailing Flap Position Indicating System
  > WHEN DEPARTING, FLAPS FAIL AT 18 DEGREES. BOTH FLAP INOP LIGHT AND FLAP FAULT LIGHT ILLUMINATED, FOLLOW ALL QRH CHECKLIST LANDING. ECU FAULT LED NR 4 SHOWING C/W AMM, FLAPS RESET. FAULT LED 1 AND 2 AND 8 SHOWING, ACCOMPLISHED SL2 RESET. RAN FLAPS 0-33 DEGR
- [SDR A6WA200460025](https://openairdocs.org/sdr/A6WA200460025.md): Bolt · corroded · Jul 17, 2004 · N607AW · Bac 146200A · Fasteners
  > FOUND CORROSION ELEVATOR HINGE A-FRAME ATTACHMENT BOLTS TWO EACH. REPLACED NEW. (M)
- [SDR A6WA200460027](https://openairdocs.org/sdr/A6WA200460027.md): Angle · corroded · Jul 17, 2004 · N607AW · Bac 146200A · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON INTERCOSTAL AT CETNER JOINT PLATE 80 INCHES FROM DOOR 1L. REPLACED ANGLE, IAW BAE SRM 51-42-00 AND 51-23-00. (M)
- [SDR A6WA200460015](https://openairdocs.org/sdr/A6WA200460015.md): Flap Track · worn · May 12, 2004 · N607AW · Bag BAE146200A · Trailing Edge Flaps
  > NR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES.033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 607-1907002. MAINTENANCE REMOVED LOWER CARRIAGE NR 2 LEFT. ROLLERS REPLACED IAW CMM 57-50-22. CARRIAGE REINSTALLED IAW AMM 2
- [SDR A6WA200460030](https://openairdocs.org/sdr/A6WA200460030.md): Intercostal · cracked · May 11, 2004 · N607AW · Bac 146200A · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 22/23 AT STRINGER 21 RIGHT IN FORWRAD CARGO COMPARTMENT. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-23-00, 51-42-00 AND 51-43-00. (M)
- [SDR A6WA200460031](https://openairdocs.org/sdr/A6WA200460031.md): Intercostal · cracked · May 11, 2004 · N607AW · Bac 146200A · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 21/22 AT STRINGER 21 RT IN FORWARD CARGO BAY. MAINTENANCE REPLACED INTERCOSTAL IAW SRM 51-23-00, 51-42-00, AND 51-43-00. (M)
- [SDR A6WA200460028](https://openairdocs.org/sdr/A6WA200460028.md): Floor Support · corroded · May 10, 2004 · N607AW · Bac 146200A · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR SUPPORT MEMBER ADJACENT TO FLOORBEAM 15.52 INCHES FROM DOOR 1L. MAINTENANCE REPLACED JOINT PLATE WITH MANUFACTURED REPAIR PART IAW BAE SRM 51-20
- [SDR A6WA200460029](https://openairdocs.org/sdr/A6WA200460029.md): Stringer · corroded · May 10, 2004 · N607AW · Bac 146200A · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON CENTER LINE STRINGER IN FORWARD CARGO PIT BETWEEN FORWARD AND AFT RADIO ALT ANTENNAS. MAINTENANCE REPLACED STRINGER WITH MANUFACTURED REPAIR PART IAW SRM.
- [SDR A6WA200460001](https://openairdocs.org/sdr/A6WA200460001.md): Apu · inoperative · Jan 5, 2004 · N607AW · Bac 146200A · APU Core Engine
  > SMOKE IN CABIN WHEN APU IS SUPPLYING AIR TO PACKS. MAINTENANCE PERFORMED PACK BURNOUT AND REMOVED AND REPLACED APU. (M)
- [SDR A6WA200360070](https://openairdocs.org/sdr/A6WA200360070.md): Stringer · corroded · Dec 12, 2003 · N607AW · Bac 146200A · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 34R HAS CORROSION. MAINTENANCE REPAIRED STRINGER 34R BETWEEN FRAMES 20B AND 21 IAW BAE FAX BARA/AVR/6609/03-DC AND IAW BAE SRM 51-43-00. (M)
- [SDR A6WA200360069](https://openairdocs.org/sdr/A6WA200360069.md): Skin · damaged · Dec 9, 2003 · N607AW · Bag BAE146200A · Fuselage Main, Plate/Skin
  > FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVIT LOCATIONS. MAINTENANCE CUT OUT DAMAGE TO SKIN IAW BAE FAX BARA/AVR/6603/03-DC. NDT HFEC CARRIED OT IAW BAE FAX BARA/AVR/6603/03-DC, NO CRACKS NOTED.
- [SDR A6WA200360067](https://openairdocs.org/sdr/A6WA200360067.md): Structure · damaged · Dec 9, 2003 · N607AW · Bag BAE146200A · Trailing Edge Flaps
  > RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. BUSHING LOCALLY MANUFACTURED AT AAO AND CAD PLATED IAW BAE FAX BARA/AVR/6605/03-DC. BUSHING INSTALLED IAW FLAP EO EO2/021/657. (M)
- [SDR A6WA20030069](https://openairdocs.org/sdr/A6WA20030069.md): Skin · cracked · Dec 9, 2003 · N607AW · Bac 146200A · Fuselage Main, Plate/Skin
  > FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVET LOCATIONS. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF FAX 1734-6070004. (M)
- [SDR A6WA200360068](https://openairdocs.org/sdr/A6WA200360068.md): Flap Track · worn · Dec 9, 2003 · N607AW · Bac 146200A · Trailing Edge Flaps
  > RT NR 1 FLAP TRACK WEAR UPPER AND LOWER RAILS OUTBOARD FACE. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1734-6070003. LPI C/O ON BLENDED FLAP TRACK AS REQUIRED IAW BARA/AVR/6606/03-DC, NO CRACKS FOUND. (M)
- [SDR A6WA200350067](https://openairdocs.org/sdr/A6WA200350067.md): Structure · damaged · Dec 9, 2003 · N607AW · Bac 146200A · Trailing Edge Flaps
  > RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 134-6070002. (M)
- [SDR A6WA200360064](https://openairdocs.org/sdr/A6WA200360064.md): Wire · burned · Oct 29, 2003 · N607AW · Bac 146200A · Electrical Power System Wiring
  > APU GENERATOR INOPERATIVE. DURING MAINTENANCE CORRECTIVE ACTION FOUND 3 APU GENERATOR WIRES IN FORWARD CARGO BAY CEILING BURNED AND EVIDENCE OF ARCHING ON CARGO LINER. MAINTENANCE REPLACED THE 3 PHASE APU GENERATOR WIRES AND CRIMP SLEEVES, PER BAE MM 24-00-0
- [SDR A6WA200360039](https://openairdocs.org/sdr/A6WA200360039.md): Skin · cracked · Sep 22, 2003 · N607AW · Bac 146200A · Fuselage Main, Plate/Skin
  > RIGHT FUSELAGE SKIN AT FRAME 32 ABOVE STRINGER 19 HAS A.0250 INCH CRACK ORIGINATING AT FASTENER. REPAIR I/P. (M)
- [SDR A6WA200360004](https://openairdocs.org/sdr/A6WA200360004.md): Fuel Control · malfunctioned · Mar 28, 2003 · N607AW · Bac 146200A · Fuel Controlling System
  > AT FL280, OAT -40 DEGREES C, TMS OFF, ANY REDUCTION IN POWER OF NR 3 ENGINE FUEL FLOW WOULD DROP TO 300 NR A FEW SECONDS. OTHER ENGINE INSTRUMENTS WOULD DROP ACCORDINGLY. REMOVED AND REPLACED NR 3 FUEL CONTROL ASSEMBLY. OPS AND LEAK CHECKS GOOD AT THIS TIME
- [SDR A6WA200100027](https://openairdocs.org/sdr/A6WA200100027.md): Slide · unserviceable · Mar 29, 2001 · N607AW · Bag BAE146200A · Escape Slide
  > FOUND THE FWD PAX DOOR EVACUATION SLIDE CABLE RELEASE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPAIRED EVACUATION SLIDE.
- [SDR A6WA200100013](https://openairdocs.org/sdr/A6WA200100013.md): Slide · will not test · Jan 26, 2001 · N607AW · Bag BAE146200A · Escape Slide
  > LIGHTS ON EMERGENCY ESCAPE SLIDE NOT ILLUMINATE DUE TO PIN IN BATTERY NOT BEING PULLED OUT UPON DEPLOYMENT. SNAP THAT HOLDS PIN LANYARD BECAME DETACHED INSTEAD. MAINTENANCE REMOVED AND REPLACED EMERGENCY SLIDE ASSEMBLY.
- [SDR A6WA9900082](https://openairdocs.org/sdr/A6WA9900082.md): Switch · dirty · Jul 24, 1999 · N607AW · Bag BAE146200A · Door Warning System
  > LOWER DOOR NOT SHUT ON MWS PANEL, CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF AND VERIFIED ALL DOORS SHUT. CLEANED AND INSPECTED LOWER DOOR SWITCHES, ALL CHECKED GOOD. (X)
- [SDR A6WA9900046](https://openairdocs.org/sdr/A6WA9900046.md): Bearing · failed · May 27, 1999 · N607AW · Bag BAE146200A · Wheel/Ski/Float
  > REMOVED NR 1 TIRE ASSY, FOUND NR 1 WHEEL INNER BEARING SEIZED ONTO THE AXEL. REMOVED AND REPLACED LEFT MLG AXEL, WHEELS AND NR 1 HEAT PACK AND BRAKE. NR 1 BRAKE P/N AHA1413, SN HB182 TMS 2861. CYCLES 3,131. NR 1 CARBON HEAT PACK PN AH09068, SN AWAC170. TM
- [SDR 99ZZZM792](https://openairdocs.org/sdr/99ZZZM792.md): Compressor · damaged · Feb 16, 1999 · N607AW · Bag BAE146200A · Turbine Engine Compressor Section
  > NR 1 ENGINE VIBRATION 2.5 AIRBORN ENGINE SHUTDOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLADES MISSING FROM NR 3 AND NR 4 WHEEL AND DAMAGE TO NR 2 WHEEL AND SUSPECT DAMAGE TO NR 1 WHEEL. AIRCRAFT TO BE FERRIED TO ATW. (M)
- [SDR 99ZZZX2697](https://openairdocs.org/sdr/99ZZZX2697.md): Compressor · failed · Feb 6, 1999 · N607AW · Bag BAE146200A · Turbine Engine Compressor Section
  > DEN - FLT 595 - NR 1 ENGINE: VIBRATION 2.5 AIR-BORN. ENGINE SHUT DOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLADES MISSING FROM NR 3 AND NR 4 WHEEL AND DAMAGE TO NR 2 WHEEL AND SUSPECT DAMAGE TO NR 1 WHEEL. AIRCRAFT TO BE FERRIED TO ATW. ACFT TT: 1
- [SDR 99ZZZX2698](https://openairdocs.org/sdr/99ZZZX2698.md): Pin · failed · Jan 23, 1999 · N607AW · Bag BAE146200A · Landing Gear Actuator
  > UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK, FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR E.O. E98/002/632. REMOVED AND REPLACED THE NLG RETRACTION JACK PIN AS REQUIRED DURING REMOVAL AND REPLACMENT OF JACK STREET. ACFT TT: 23,
- [SDR 99ZZZM551](https://openairdocs.org/sdr/99ZZZM551.md): Actuator · failed · Jan 23, 1999 · N607AW · Bag BAE146200A · Landing Gear Actuator
  > UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR EO E98/002/632. REMOVED AND REPLACED THE NLG RETRACTION JACK PIN AS REQ'D DURING REMOVING AND REPLACING OF JACK STREET. (M)
- [SDR 98ZZZM691](https://openairdocs.org/sdr/98ZZZM691.md): Trim · binds · Feb 27, 1998 · N607AW · Bag BAE146200A · Elevator Tab Control System
  > ELEVATOR TRIM BINDS AT ALL SPEEDS, ALL ALTITUDES WHEN MOVED FORWARD OF 3 ON THE TRIM INDICATOR.
- [SDR 98ZZZM692](https://openairdocs.org/sdr/98ZZZM692.md): Trim · binds · Feb 26, 1998 · N607AW · Bag BAE146200A · Elevator Tab Control System
  > AT 20,000 FT 290 KTS ELEV TRIM BINDS WHEN TRYING TO TRIM NOSE DOWN, NOSE UP FEELS NORMAL. PERFORMED ELEV TRIM CIRCUIT FRICTION TST, ALSO PERFORMED CLUTCH FRICTION TEST, INSPECTED CIRCUIT AND INTERCONNECT CIRCUIT AT ELEV, BOTH TESTS AND VISUAL ACCOMPLISHED WIT
- [SDR 98ZZZX1183](https://openairdocs.org/sdr/98ZZZX1183.md): Panel · loose · Nov 19, 1997 · N607AW · Bag BAE146200A · Wing, Plate/Skin
  > ATW - FLT 505 - ON CLIMB-OUT ACCELERATING THROUGH 240-250 KNOTS, FELT SLIGHT AIRFRAME VIBRATION. AS SPEED INCREASED, VIBRATION INCREASED. REPLACED PANEL ON RT TRAILING EDGE OF WING AND SEAL.
- [SDR 98ZZZX1188](https://openairdocs.org/sdr/98ZZZX1188.md): Retract Mech · malfunctioned · Nov 2, 1997 · N607AW · Bag BAE146200A · Trailing Edge Flap Control System
  > DEN - FLT 669 - FLAPS WOULD NOT MOVE FROM THE 24 DEGREE POSITION IN THE AIR. CLEARED FLAP FAULT AND OPS TESTED GOOD.
- [SDR 98ZZZX1189](https://openairdocs.org/sdr/98ZZZX1189.md): Air Distribution · odor · Nov 1, 1997 · N607AW · Bag BAE146200A · Air Distribution System
  > ATW - WHEN SWITCHING AIR FROM APU TO ENG AIR, NR 1 PACK GIVES A STRONG OIL BURNING SMELL FOR A FEW MINUTES THEN IT CLEARS. OPS CHECKED NR 1 PACK ON THE GROUND WITH APU AND ENG AIR, NO SMELL NOTICED.
- [SDR 98ZZZM90](https://openairdocs.org/sdr/98ZZZM90.md): Line · failed · Sep 14, 1997 · N607AW · Bag BAE146200A · Landing Gear Actuator
  > GREEN HYD SYSTEM LOW QTY AND LOW PRESS IN FLT. REPLACED HYD RETURN HOSE TO LEFT MLG RETRACTION JACK. (M)
- [SDR 98ZZZM89](https://openairdocs.org/sdr/98ZZZM89.md): Terminal Block · corroded · Aug 22, 1997 · N607AW · Bag BAE146200A · Passenger Compartment Lighting
  > TWO TERMINAL BLOCKS BELOW THE INBOARD AIRSTAIR DRIP TRAY FOR THE PAX DOOR ARE CORRODED AND NEEDS TO BE CLEANED. REPLACED TERMINAL BLOCKS AA AND AB IN ZONE 131-00-00 AND OPENED WORK CARD FOR TEST. (M)
- [SDR 98ZZZM88](https://openairdocs.org/sdr/98ZZZM88.md): Bracket · worn · Aug 18, 1997 · N607AW · Bag BAE146200A · Landing Gear Door Retract Section
  > NLG AFT DOOR STOP ASSY MATERIAL MORE THAN 50 PERCENT WORN. REPLACED DOOR STOP BRACKET. DOOR CLEARANCES TO BE CHECKED ON GEAR SWING INSTALLATION. (M)
- [SDR 98ZZZM87](https://openairdocs.org/sdr/98ZZZM87.md): Seat Rail · corroded · Aug 18, 1997 · N607AW · Bag BAE146200A · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD RIGHT I/N SEAT RAIL HAS CORROSION PAST LIMITS (FWD 23 INCHES). REMOVED 24 INCHES OF SEAT RAIL RT INBOARD FORWARD AND SPLICED IN NEW SECTION OF SEAT RAIL PER SRM 53-00-32 PAGES 202, 203 AND 204. ANODIZED REPLACEMENT PART TO MIL-A-8625F PER BAE FAX DJR
- [SDR 98ZZZM63](https://openairdocs.org/sdr/98ZZZM63.md): Track · worn · Aug 15, 1997 · N607AW · Bag BAE146200A · Trailing Edge Flaps
  > LEFT NR 1 FLAP TRACK SHOWS WEAR ON OUTBOARD SURFACES OF UPPER AND LOWER RAILS. BLENDED WORN AREAS IAW BAE ATW FAX DJR/RJ0647-97. MAX CLEARANCE WITH NEWPADS IS.092 INCH REF FAX FOR EXTENDED WEAR LIMIT.
- [SDR 98ZZZM62](https://openairdocs.org/sdr/98ZZZM62.md): Roller · corroded · Aug 15, 1997 · N607AW · Bag BAE146200A · Trailing Edge Flaps
  > LEFT FLAP NR 1 CARRIAGE ROLLER ASSY TO LICK ATTACH BOLT CORRODED. REMOVED AND REPLACED CORRODED ROLLER TO CARRIAGE ATTACH BOLT.
- [SDR 98ZZZM61](https://openairdocs.org/sdr/98ZZZM61.md): Seat Rail · corroded · Aug 15, 1997 · N607AW · Bag BAE146200A · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD LEFT.1B SEAT RAIL HAS CORROSION PAST LIMITS, APPROX 64 INCH LENGTH. REMOVED 65 INCHES FORWARD SECTION OF LEFT INBOARD SEAT RAIL ASSY AND SPLICED REPLACEMENT SEC PER SRM 53-00-32 PAGE 202, 203, 204. ANODIZED REPLACED PART PER MIL-A-8625F AND FAX BAE
- [SDR 98ZZZM60](https://openairdocs.org/sdr/98ZZZM60.md): Control Cable · corroded · Aug 13, 1997 · N607AW · Bag BAE146200A · Aileron Control System
  > RIGHT AILERON CABLES CORRODED AT BELLCRANK AT RIB NR 10. REMOVED AND REPLACED BOTH RIGHT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW BAE MM.
- [SDR 98ZZZM59](https://openairdocs.org/sdr/98ZZZM59.md): Control Cable · corroded · Aug 13, 1997 · N607AW · Bag BAE146200A · Aileron Control System
  > LEFT OUTER AILERON CONTROL CABLE HAS RUST ON OUTER CABLE QUANDRANT. REMOVED AND REPLACED BOTH LEFT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW BAE MM.
- [SDR 98ZZZM58](https://openairdocs.org/sdr/98ZZZM58.md): Stiffener · cracked · Aug 8, 1997 · N607AW · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING, TRAILING EDGE AREA AFT OF REAR SPAR HAS A CRACKED STIFFENER ON LOWER SHROUD SKIN BETWEEN WING RIBS NR 7 AND 8. REPLACED STIFFENER AND PAINTED.
- [SDR 98ZZZM57](https://openairdocs.org/sdr/98ZZZM57.md): Stiffener · cracked · Aug 7, 1997 · N607AW · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING T/E SHROUD AREA BETWEEN WING WIBS NR 8 AND 9 HAS THE TWO UPPER SKIN STIFFENERS WITH CRACKS AT THEIR FWD ENDS. REPAIRED OUTBOARD STIFFENER PER FAX JM/RJ0317/97, REPLACED INBOARD STIFFENER PER SRM ALSO REF BAE FAX RA/RJO595-97.
- [SDR 98ZZZM56](https://openairdocs.org/sdr/98ZZZM56.md): Bracket · cracked · Aug 6, 1997 · N607AW · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING T/E AREA AT WING RIB NR 8 HAS A CRACKED HYD LINE BRACKET WHICH IS ALLOWING HYD LINE TO CHAF ON THE TAIL RIB. HYD LINE IS GOING OUT OT OUTBOARD LIFT SPOILER JACK. INSPECTED LINE OK. REPLACED CRACKED BRACKET.
- [SDR 98ZZZM55](https://openairdocs.org/sdr/98ZZZM55.md): Bracket · cracked · Aug 5, 1997 · N607AW · Bag BAE146200A · Engine Cowling System
  > NR 4 ENGINE LEFT FAN DOOR HAS ONE BRACKET CRACKED AND ONE RIVET HEAD SHEARED ON BOTTOM SPLITTER. REPLACED ONE SHEARED RIVET HEAD AND ONE BRACKET ON NR 4 ENGINE LEFT FAN DOOR AS WRITTEN ABOVE.
- [SDR 98ZZZM54](https://openairdocs.org/sdr/98ZZZM54.md): Angle · cracked · Aug 5, 1997 · N607AW · Bag BAE146200A · Fuselage Miscellaneous Structure
  > CENTER MLG BAFFLE UPPER ATTACHMENT ANGLE CRACKED THROUGH TWO RIVETS 1.5625 INCHES IN LENGTH. REPAIR/REPLACE NO LATER THAN 34926 TCA AS PER AVRO FAX DJR/RJ1322-96, ANGLE MANUFACTURED OF L166 MATERIAL. REMOVED AND REPLACED ABOVE BAFFLE ANGLE USING.040 L166 (2
- [SDR 98ZZZM53](https://openairdocs.org/sdr/98ZZZM53.md): Jamb · cracked · Aug 4, 1997 · N607AW · Bag BAE146200A · Engine Cowling System
  > NR 4 ENGINE RIGHT FAN DOOR BOTTOM EDGE MEMBER NEEDS A CRACK DRESSED OUT AND TREATED. DRESSED OUT DOOR EDGE MEMBER CRACK AT REQUESTED AT THIS TIME. REPAINTED ENTIRE AREA OF REPAIR. PERFORMED EC ON AREA ABOVE THAT WAS DRESSED OUT AND FOUND IT TO BE CRACK FREE
- [SDR 98ZZZM52](https://openairdocs.org/sdr/98ZZZM52.md): Mount Bolt · damaged · Aug 4, 1997 · N607AW · Bag BAE146200A · Elevator Structure
  > LEFT ELEVATOR NR 2 HINGE A FRAME UPPER MOUNT BOLT FAILS DETAILED VISUAL INSPECTION. REPLACED UPPER MOUNT BOLT WITH SERVICEABLE BOLT.
- [SDR 98ZZZM51](https://openairdocs.org/sdr/98ZZZM51.md): Mount Plate · cracked · Aug 2, 1997 · N607AW · Bag BAE146200A · Drag Control System
  > LIFT SPOILER VALVE MOUNT PLATE CRACKED IN RT WING ROOT. REMOVED VALVE, REPLACED PLATE AND REINSTALLED VALVE, GEN W/C DO LEAK AND OPS CHECK.
- [SDR 98ZZZM50](https://openairdocs.org/sdr/98ZZZM50.md): Stiffener · cracked · Aug 1, 1997 · N607AW · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE AREA AFT OF REAR SPAR BETWEEN WING RIBS NR 7 AND 8 HAS AN UPPER SKIN STIFFENER THATS CRACKED AT FORWARD END. REPAIRED IAW ATTACHED FAXES RA/RJO595-97 AND OTHERS RELATED.
- [SDR 97ZZZM789](https://openairdocs.org/sdr/97ZZZM789.md): Smoke Hood · damaged · Jun 30, 1997 · N607AW · Bag BAE146200A · Portable Oxygen System
  > REQ MAINTENANCE CHECK, AFT PBE FOR SERVICEABILITY. REMOVED AND REPLACED AFT PBE MAS ASSY. (M)

Next page: https://openairdocs.org/deregistered/N607AW-2006-07-20/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 = 'N607AW' AND deregistration_id = 'N607AW-2006-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N607AW-2006-07-20/reports

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