# Service difficulty reports: N709AS, cancelled Sep 5, 2018

A list on [N709AS, cancelled Sep 5, 2018](https://openairdocs.org/deregistered/N709AS-2018-09-05.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 4 · 184 reports

- [SDR FOTR20180830005](https://openairdocs.org/sdr/FOTR20180830005.md): Fitting · cracked · Aug 30, 2018 · N709AS · Boeing 737490 · Cargo/Baggage Doors
  > DURING HFEC OPEN HOLE INSPECTION OF MCD LATCH ASSY. FASTENER HOLES, INDICATION NPTED AT STA 420 FASTENER HOLE NR 2F.
- [SDR FOTR201808209003](https://openairdocs.org/sdr/FOTR201808209003.md): Spar · cracked · Aug 19, 2018 · N709AS · Boeing 737490 · Wing Main, Frame Structure
  > RT WING REAR SPAR RSS 218 CRACKED AT INBD SIDE OF MLG SUPPORT FITTING.
- [SDR FOTR201808209002](https://openairdocs.org/sdr/FOTR201808209002.md): Support Angle · corroded · Aug 19, 2018 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > BS 540 BETWEEN STRINGERS 27R - 28R SUPPORT ANGLE HAD CORROSION.
- [SDR FOTR2018080800001](https://openairdocs.org/sdr/FOTR2018080800001.md): Frame · cracked · Jul 6, 2018 · N709AS · Boeing 737490 · Fuselage Main, Frame
  > FORWARD CARGO BAY, BS 500B FRAME WAS CRACKED AT THE INBD SIDE OF WIRE PENETRATION HOLE.
- [SDR ASAA2018020123399](https://openairdocs.org/sdr/ASAA2018020123399.md): Screw · sheared · Feb 1, 2018 · N709AS · Boeing 737490 · Passenger/Crew Doors
  > CREW COULD NOT OPEN L1 DOOR AFTER LANDING. GROUNDED - YES. FOUND SCREW SHEARED ON LOWER RADIUS LINK OF L1 DOOR GUIDE ARM. REMOVED RADIUS LINK OUT OF THE WAY AND WAS ABLE TO OPEN DOOR. REMOVED AND REPLACED RADIUS LINK ATTACHING HARDWARE ON GUIDE ARM REF CMM 52-
- [SDR ASAA2017111022533](https://openairdocs.org/sdr/ASAA2017111022533.md): Sign · broken · Nov 10, 2017 · N709AS · Boeing 737490 · Emergency Lighting
  > EXIT SIGN ABOVE THE ENTRY TO FLIGHT DECK IS BROKEN. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN COVER THAT WAS BROKEN.
- [SDR ASAA2017091322121](https://openairdocs.org/sdr/ASAA2017091322121.md): Frame · cracked · Sep 13, 2017 · N709AS · Boeing 737490 · Fuselage Main, Frame
  > RIGHT OTBD BS 727 FRAME CRACKED, STRINGER 18A. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW AD20122304-400-53-011R, AND AD20122304-400-53-8.
- [SDR ASAA2017091322063](https://openairdocs.org/sdr/ASAA2017091322063.md): Tee Fitting · cracked · Sep 13, 2017 · N709AS · Boeing 737490 · Fuselage Main, Structure
  > FWD GALLEY DOOR CUTOUT NR 1 DOOR STOP TEE CRACKED IN RADIUS BS 333, STRINGER 8. ACFT GROUNDED. REMOVED AND REPLACED THE TEE IAW SRM 51-40-02.
- [SDR ASAA2017080321547](https://openairdocs.org/sdr/ASAA2017080321547.md): Guide Arm · damaged · Aug 3, 2017 · N709AS · Boeing 737490 · Passenger/Crew Doors
  > RAMP REPORTED UNABLE TO OPEN THE L1 DOOR. ACFT GROUNDED. ATTEMPTED TO OPEN DOOR, NO LUCK. DOOR UNLATCHES, CRACKS OPEN MAKING A CRACKLING NOISE AND BINDS. FOUND BOTTOM RADIUS LINK KEY WASHER AND SCREW MISSING WHICH CAUSED BINDING ON L1 DOOR GUIDE ARM. REMOV
- [SDR ASAA2017073123693](https://openairdocs.org/sdr/ASAA2017073123693.md): Skin · cracked · Jul 31, 2017 · N709AS · Boeing 737490 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR SKIN CRACKED, UPPER AFT CORNER OF HANDLE CUT OUT. ACFT GROUNDED. INSTALLED A REPAIR DOUBLER IAW SRM 52-00-01-2R-2.
- [SDR ASAA2017052220920](https://openairdocs.org/sdr/ASAA2017052220920.md): Stop Fitting · gouged · May 22, 2017 · N709AS · Boeing 737490 · Cargo/Baggage Doors
  > FWD CARGO DOOR FWD LOWER FITTING DAMAGE IN PREVIOUS BLENDED AREA OUT OF LIMITS OF IAW SRM 52-30-02-1A-1. ACFT GROUNDED. REPLACED FWD LOWER STOP FITTING IAW SRM 51-40-02, AND DWG 65-46921.
- [SDR ASAA2016040416271](https://openairdocs.org/sdr/ASAA2016040416271.md): Intercostal · cracked · Apr 4, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY INTERCOSTAL BS 420-440, STR 26R IS CRACKED, FOUND UPON REMOVAL OF TRANSITIION PANEL. ACFT GROUNDED. R & R CRACKED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016033016464](https://openairdocs.org/sdr/ASAA2016033016464.md): Stringer Splice · corroded · Mar 30, 2016 · N709AS · Boeing 737490 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY STRINGER SPLICE 21R AT BS 907 IS CORRODED. ACFT GROUNDED. R & R THE STRINGER SPLICE AT BS 907 IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016033016276](https://openairdocs.org/sdr/ASAA2016033016276.md): Strap · cracked · Mar 30, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FLOORBEAM STABILIZER STRAP BL0 IS CRACKED THROUGH AT BS 312. ACFT GROUNDED. R & R STRAP IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016032816556](https://openairdocs.org/sdr/ASAA2016032816556.md): Stringer · corroded · Mar 28, 2016 · N709AS · Boeing 737490 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R HAS MULTIPLE AREAS OF CORROSION AT BS 986. ACFT GROUNDED. R & R THE STRINGER IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016032816329](https://openairdocs.org/sdr/ASAA2016032816329.md): Web · corroded · Mar 28, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > LATERAL TRACK AT BS 807, LBL 50 CORRODED ON LOWER SIDE. ACFT GROUNDED. REMOVED AND REPLACED WEB UNDERNEATH LATERAL TRACK AT BS 807, LBL 50 IAW SRM 51-40-02-0G-0, W 2, O.071", R 0.58", L 4, D.013".
- [SDR ASAA2016032816274](https://openairdocs.org/sdr/ASAA2016032816274.md): Intercostal · cracked · Mar 28, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BS 312 TO BS 328 AT LBL45, CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016032716553](https://openairdocs.org/sdr/ASAA2016032716553.md): Frame · cracked · Mar 27, 2016 · N709AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME AT BS 344 HAS A CRACK INDICATION AT BS 4 RT LOWER FWD HOLE AT SPLICE. ACFT GROUNDED. REPAIRED DAMAGE TO FRAME IAW EA 400-53EA-17039. THIS REPAIR HAS A REINSPECT THRESHOLD OF 8,000 FLT. CYCLES AFTER MODIFICATION WITH A REPAIR INTERVAL OF 8,000 FLT. CY
- [SDR ASAA2016032616443](https://openairdocs.org/sdr/ASAA2016032616443.md): Cargo Track · corroded · Mar 26, 2016 · N709AS · Boeing 737490 · Fuselage, Seat/Cargo Attach Fittings
  > AFT PIT CARGO TRACK RBL 13 AT BS 945 IS CORRODED. ACFT GROUNDED. CORRODED TRACK IS FOUND OUT OF LIMITS. R & R DAMAGE SECTION OF TRACK IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016032416335](https://openairdocs.org/sdr/ASAA2016032416335.md): Strap · cracked · Mar 24, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > MCD STRAP AT BS 460, STR 20L CRACKED. ACFT GROUNDED. R & R INNER WEB STRAP IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016032416334](https://openairdocs.org/sdr/ASAA2016032416334.md): Strap · cracked · Mar 24, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > MCD STRAP AT BS 400, SR 20L CRACKED. ACFT GROUNDED. R & R INNER WEB STRAP IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016032416333](https://openairdocs.org/sdr/ASAA2016032416333.md): Strap · cracked · Mar 24, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > MCD STRAP AT BS 420, STR 20L CRACKED. ACFT GROUNDED. R & R INNER WEB STRAP IAW SRM 51-42-02-0G-0.
- [SDR ASAA2016032316398](https://openairdocs.org/sdr/ASAA2016032316398.md): Frame · cracked · Mar 23, 2016 · N709AS · Boeing 737490 · Fuselage Main, Frame
  > LEFT FRAME, STA 500E IS CRACKED AT.50 HOLE BETWEEN STR 20 AND 21 LT. ACFT GROUNDED. REPAIRED DAMAGE TO FRAME IAW SRM 53-00-07-2R-13, REPAIR 13. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 66,000 TOTAL ACFT CYCLES REFER TO SRM 53-00-07-2R-13,
- [SDR ASAA2016032316215](https://openairdocs.org/sdr/ASAA2016032316215.md): Intercostal · cracked · Mar 23, 2016 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED IN RADIUS AT STR 14 RT AT BS 277. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR ASAA2015022810827](https://openairdocs.org/sdr/ASAA2015022810827.md): Fitting · corroded · Feb 28, 2015 · N709AS · Boeing 737490 · Fuselage, Door Hinge
  > L1 DOOR LWR HINGE, UPPER BEARING PLATE SUPPORT STRUCTURE CORRODED AT FASTENERS, FOUND OK TO INSTALL. ACFT GROUNDED. R & R LOWER HINGE SUPPORT FITTING IAW SRM 51-40-02 0G 0, W 1, O.100, R 0, L 1, D 100 PERCENT.
- [SDR ASAA2015021510757](https://openairdocs.org/sdr/ASAA2015021510757.md): Angle · cracked · Feb 15, 2015 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERNAL ANGLE BELOW STRINGER 12 ON FWD SIDE OF RT GALLEY DOOR IS CRACKED NDT VERIFIED. ACFT GROUNDED. R & R INTERNAL ANGLE BELOW STRINGER 12 ON FWD SIDE OF RT GALLEY DOOR IAW SRM 51-40-02-0G-0.
- [SDR ASAA2015021510747](https://openairdocs.org/sdr/ASAA2015021510747.md): Angle · cracked · Feb 15, 2015 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERNAL ANGLE BELOW STRINGER 11 ON FWD SIDE OF RT GALLEY DOOR CUTOUT IS CRACKED, NDT VERIFIED. ACFT GROUNDED. R & R THE ANGLE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2015021510746](https://openairdocs.org/sdr/ASAA2015021510746.md): Angle · cracked · Feb 15, 2015 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERNAL ANGLE ABOVE STRINGER 10 ON FWD SIDE OF RT GALLEY DOOR CUT OUT IS CRACKED NDT VERIFIED. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2015021110825](https://openairdocs.org/sdr/ASAA2015021110825.md): Channel · corroded · Feb 11, 2015 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT WASTE WATER DRAIN MAST MIDDLE ATTACH FASTNER HOLE HAS LIGHT SURFACE CORR ON INTERNAL SIDE. REF AD 20122314-400-53 STE4P 14 CORR WAS FOUND CONTACT ENG TO OBTAIN AMOC REPAIR. GROUNDED - YES. REMOVED AND REPLACED AFT WASTE WATER DRAIN MAST MIDDLE SUPPORT CHAN
- [SDR ASAA2015011610289](https://openairdocs.org/sdr/ASAA2015011610289.md): Lens · broken · Jan 16, 2015 · N709AS · Boeing 737490 · Emergency Lighting
  > L1 DOOR FLOOR EMERGENCY EXIT LIGHT COVER LENS BROKEN. ACFT GROUNDED. REPLACED L1 DOOR FLOOR EMERGENCY EXIT LIGHT COVER LENS REF AMM 33-51-81-962-011. OPS CHECK GOOD.
- [SDR ASAA2013102496517](https://openairdocs.org/sdr/ASAA2013102496517.md): Web · cracked · Oct 24, 2013 · N709AS · Boeing 737490 · APU Cowling/Containment
  > APU UPPER SHROUD RT SIDE EDGE HAS A CRACK BY AFT LATCH FITTING. ACFT GROUNDED. REPAIRED APU UPPER SHROUND RT SIDE EDGE IAW EA 400-49EA-11534.
- [SDR ASAA2013102496516](https://openairdocs.org/sdr/ASAA2013102496516.md): Web · cracked · Oct 24, 2013 · N709AS · Boeing 737490 · APU Cowling/Containment
  > APU UPPER SHROUD AIR INLET CUTOUT WEB EDGE BENT AND CRACKED. ACFT GROUNDED. REPAIRED APU UPPER AIR INLET CUTOUT WEBS IAW EA 400-49EA-11524.
- [SDR ASAA2013102196318](https://openairdocs.org/sdr/ASAA2013102196318.md): Skin · cracked · Oct 21, 2013 · N709AS · Boeing 737490 · Wing, Plate/Skin
  > LEFT WING FIXED L/E IS CRACKED AT NR 2 SLAT ACTUATOR CUTOUT. ACFT GROUNDED. REMOVED ACTUATOR CURTAIN, REPAIRED CRACK IAW SRM 57-41-01-2R-7 AND REINSTALLED ACTUATOR CURTAIN ALSO SRM 57-41-01-2R-7.
- [SDR ASAA2013102196317](https://openairdocs.org/sdr/ASAA2013102196317.md): Skin · delaminated · Oct 21, 2013 · N709AS · Boeing 737490 · Leading Edge Devices
  > LEFT WING, NR 2 SLAT INBD T/E IS DELAMINATED. ACFT GROUNDED. REPAIRED NR 2 SLAT INBD T/E IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2013102196300](https://openairdocs.org/sdr/ASAA2013102196300.md): Skin · cracked · Oct 21, 2013 · N709AS · Boeing 737490 · Wing, Plate/Skin
  > LEFT WING FIXED L/E CRACKED AT NR 3 SLAT ACTUATOR CUTOUT. ACFT GROUNDED. REPAIRED NR 3 SLAT ACTUATOR CUTOUT IAW SRM 51-70-14-06-0 AND 57-41-01-2R-7, FIG 201.
- [SDR ASAA2013101996267](https://openairdocs.org/sdr/ASAA2013101996267.md): Floorbeam · cracked · Oct 19, 2013 · N709AS · Boeing 737490 · Fuselage Main, Floor Beam
  > MAIN CARGO DECK FLOOR SUPPORT STRUCTURE RT BS 639, STUB BEAM INNER CHORD EVIDENCE OF BEING CRACKED AT LWR ATTACHMENT REPAIRED RT STUB BEAM INNER CHORD BS 639 IAW DWG A-5310025284.
- [SDR ASAA2013040894402](https://openairdocs.org/sdr/ASAA2013040894402.md): Guide Arm · out of adjust · Apr 8, 2013 · N709AS · Boeing 737490 · Passenger/Crew Doors
  > L1 DOOR HARD TO CLOSE. ADJUSTED L-1 DOOR GUIDE ARM REF AMM 52-11-21. ACCOMPLISHED FWD ENTRY DOOR TEST REF AMM 52-11-00. OPS CK GOOD.
- [SDR ASAA2013021493923](https://openairdocs.org/sdr/ASAA2013021493923.md): Door · lack of lube · Feb 14, 2013 · N709AS · Boeing 737490 · Passenger/Crew Doors
  > L1 DOOR HARD TO CLOSE. RETORQUED UPPER SNUBBER DOOR ATTACH BRACKET. CLEANED AND LUBED L1 DOOR LATCH CRANK, GUIDE PLATES, GUIDE ARM ROLLER PIN, COUNTER BALANCE BEARING, SNUBBER ABD GUIDE PIN, AND LOWER HINGE REF AM 12-25-21. OPS NORMAL.
- [SDR ASAA2012072092561](https://openairdocs.org/sdr/ASAA2012072092561.md): Frame Splice · damaged · Jul 2, 2012 · N709AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME SPLICE AT BS 328, STR 1 HAS ONLY 3 FASTENERS ENGAGED, THE 4TH HAS BEEN TRIMMED AROUND. REPAIRED IAW EA 400-53EA-08424.
- [SDR ASAA1149680](https://openairdocs.org/sdr/ASAA1149680.md): Module · failed · May 20, 2011 · N709AS · Boeing 737490 · Landing Gear Retraction/Extension System
  > RIGHT MAIN LANDING GEAR SLOW TO EXTEND. RIGHT GEAR RED REMAINED RED FOR 30 SECONDS AFTER OTHER GEAR SHOWED GREEN. DURING GO AROUND A "KLUNK" WAS HEARD AND FELT THEN INDICATED DOWN. GEAR WAS DOWN DURING RETURN TO AIRPORT. HYDRAULIC PRESSURE WAS NORMAL. SELE
- [SDR ASAA1149543](https://openairdocs.org/sdr/ASAA1149543.md): Skin · damaged · Apr 22, 2011 · N709AS · Boeing 737490 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STABILIZER LEADING EDGE UPPER SKIN CHAFED AND PUNCTURED AT L/E STA 133.15. REMOVED DAMAGED LEADING EDGE REPAIRED IAW B737 400 SRM 55 10 01 REPAIR 12 FIG 202 AND INSTALLED IAW B737 400 AMM 20 50 11 912 202.
- [SDR ASAA1149490](https://openairdocs.org/sdr/ASAA1149490.md): Skin · dented · Apr 20, 2011 · N709AS · Boeing 737490 · Trailing Edge Flaps
  > RIGHT WING I/B FORE FLAP LOWER SURFACE HAS DENT WITH CREASE 21 INCHES FROM I/B EDGE AND 3.25 INCHES FROM TRAILING EDGE. REPAIRED DAMAGE AREA OF THE RIGHT WING I/B FORE FLAP LOWER SURFACE IAW B737 400 SRM 51 70 10 REPAIR 4.
- [SDR ASAA1149500](https://openairdocs.org/sdr/ASAA1149500.md): Baffle · cracked · Apr 19, 2011 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT BAFFLE CRACKED BETWEEN BS 400 AND 420 STR 26L. REMOVED AND REPLACED DAMAGED BAFFLE IAW B737 400 SRM 51 40 02.
- [SDR ASAA1149483](https://openairdocs.org/sdr/ASAA1149483.md): Frame · corroded · Apr 19, 2011 · N709AS · Boeing 737490 · Fuselage Main, Frame
  > FOUND HOLE IN EXISTING FRAME LOWER FLANGE FORWARD CARGO BAY STA 500G FRAME CORRODED BETWEEN STR 27L- 26L. REMOVED OLD REPAIR, FABRICATED NEW REPAIR AND INSTALLED IAW B737 400 SRM 51 40 02 AND SRM 53 00 07 FIG 201.
- [SDR ASAA1149482](https://openairdocs.org/sdr/ASAA1149482.md): Frame · corroded · Apr 19, 2011 · N709AS · Boeing 737490 · Fuselage Main, Frame
  > FORWARD CARGO BAY STA 500G FRAME CORRODED BETWEEN STR 26R AND 27R. REPAIRED THE 500G FRAME IAW B737 400 SRM 53 00 07 FIG 201. REPAIR IS CATEGORY "B" REPAIR AND REQUIRES INSPECTION AT 66000 TOTAL FLIGHT CYCLES.
- [SDR ASAA1149404](https://openairdocs.org/sdr/ASAA1149404.md): Intercostal · broken · Apr 3, 2011 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 460 TO BS 480 STR 26L BROKEN. REMOVED INTERCOSTAL FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.
- [SDR ASAA1149505](https://openairdocs.org/sdr/ASAA1149505.md): Bulkhead · corroded · Apr 1, 2011 · N709AS · Boeing 737490 · Fuselage Main, Bulkhead
  > WHILE CLEANING FORWARD SIDE OF AFT PRESSURE BULKHEAD FOR THE RESTORATION CARD FOUND CORROSION AROUND THE RIVETS JUST TO THE LEFT OF BL 0. REMOVED CORROSION, CUTOUT LOWER SKIN FOR WEB ACCESS REMOVED STRINGER END FITTING. FABRICATED SKIN DOUBLER AND WEB DOUBLE
- [SDR ASAA1149504](https://openairdocs.org/sdr/ASAA1149504.md): Stiffener · corroded · Mar 31, 2011 · N709AS · Boeing 737490 · Fuselage Main, Bulkhead
  > CORROSION ON BL 0 STIFFENER AT BS 1016 (AFT PRESSURE BULKHEAD). REMOVED CORRODED STIFFENER AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 5300.
- [SDR ASAA1149503](https://openairdocs.org/sdr/ASAA1149503.md): Trans Panel · corroded · Mar 30, 2011 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY LEFT AFT TRANSITION PANEL BETWEEN BS 500B AND 500G IS CORRODED IN MULTIPE AREAS. FABRICATED REPLACEMENT TRANSITION PANEL AND INSTALLED IAW B737 400 SRM 51 40 05 AND 51 40 02.
- [SDR ASAA1149502](https://openairdocs.org/sdr/ASAA1149502.md): Trans Panel · gouged · Mar 30, 2011 · N709AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY LEFT FORWARD TRANSITION PANEL BS 420 HAS 3 GOUGES FABRICATED REPLACEMENT TRANSITION PANEL AND INSTALLED IAW B737 400 SRM 51 40 05 AND 51 40 02.

Next page: https://openairdocs.org/deregistered/N709AS-2018-09-05/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 = 'N709AS' AND deregistration_id = 'N709AS-2018-09-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N709AS-2018-09-05/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.