# Service difficulty reports: N703AS, cancelled Nov 28, 2018

A list on [N703AS, cancelled Nov 28, 2018](https://openairdocs.org/deregistered/N703AS-2018-11-28.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 · 183 reports

- [SDR ASAA2016050416624](https://openairdocs.org/sdr/ASAA2016050416624.md): Lamp · failed · May 4, 2016 · N703AS · Boeing 737490 · Emergency Lighting
  > DOOR EMERGENCY EXIT SIGN LAMPS INOPERATIVE, ACFT GROUNDED. REPLACED THE LAMPS. OPS CHECKED NORMAL.
- [SDR ASAA2015100113552](https://openairdocs.org/sdr/ASAA2015100113552.md): Doubler · cracked · Oct 1, 2015 · N703AS · Boeing 737490 · Fuselage Main, Plate/Skin
  > L2 DOOR CUTOUT BEARSTRAP IS CRACKED AT THE FWD LOWER RADIUS. ACFT GROUNDED. REPAIRED L2 DOORWAY CUTOUT FWD, LOWER BEAR STRAP IAW SRM 53-00-01-2R-32, DETAIL IV. THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 66,000 FLT. CYCLES AFTER AIRPLANE DELIVERY
- [SDR ASAA2015100113536](https://openairdocs.org/sdr/ASAA2015100113536.md): Stiffener · corroded · Oct 1, 2015 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > APU TORQUE BOX CUTOUT AT 10888 BULKHEAD INBD STIFFENER FLANGE CORRODED. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08-1A-1, FIG 11. NOTED G DETAIL VI R & R STIFFENER IAW SRM 51-40-02-0G-0, PARA 4, W.75", O
- [SDR ASAA2015100113438](https://openairdocs.org/sdr/ASAA2015100113438.md): Intercostal · corroded · Oct 1, 2015 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRUCTURE AT APPROXIMATELY BS 360 JUST AFT OF G2 INBD GALLEY MOUNT IS CORRODED. ACFT GROUNDED. REAMED HOLE FOR NUTPLATE ON FLOOR SUPPORT STRUCTURE AT APPROXIMATELY BS 360 JUST AFT OF G-2 INBD GALLEY MOUNT TO.261, CORROSION STIL EXISTS, OUT OF L
- [SDR ASAA2015100113525](https://openairdocs.org/sdr/ASAA2015100113525.md): Door Sill · corroded · Oct 1, 2015 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > L1 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. BLENDED CORRODED AREAS ON L1 MOPSILL, INNER CHORD OUT OF LIMITS, REMOVED AND INSTALLED NEW MOPSILL, INNER CHORD IAW SRM 53-10-15-1A-1, FIG 101, DETAIL IX, 51-40-02-0G-0, W 1.0, O.090, R.076
- [SDR ASAA2015093013594](https://openairdocs.org/sdr/ASAA2015093013594.md): Floorbeam · corroded · Sep 30, 2015 · N703AS · Boeing 737490 · Fuselage Main, Floor Beam
  > BS 986 FLOORBEAM UPPER HORIZONTAL FLANGE HAS AREAS OF CORROSION. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 400, 53EA 15973.
- [SDR ASAA2015093013593](https://openairdocs.org/sdr/ASAA2015093013593.md): Stringer · corroded · Sep 30, 2015 · N703AS · Boeing 737490 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R AT BS 986 HAS LARGE AREA OF CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW STIFFENER IAW SRM 51-40-02-0G-0, PARA 4 AND 7D SRM 51-40-05-0
- [SDR ASAA2015093013533](https://openairdocs.org/sdr/ASAA2015093013533.md): Frame · corroded · Sep 30, 2015 · N703AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME AT BS 992 HAS AREAS OF CORRODED JUST ABOVE L2 MOPSILL. ACFT GROUNDED. REPAIRED FRAME IAW EA 400 53EA, 15969. THIS IS A CAT B REPAIR WITH TRACKING IAW 400, 53DTI, 15970. INSPECTION THRESHOLD OF 66,000 FLT CYCLES, CURRENT FLT CYCLES AT TIME OF REPAIR IS
- [SDR ASAA2015093013493](https://openairdocs.org/sdr/ASAA2015093013493.md): Door Sill · corroded · Sep 30, 2015 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > L2 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. R & R MOPSILL IAW SRM 51-40-02-0G-0 AND DWG NR 65-52878, W 5", O.071", R.060, L 1", D.011".
- [SDR ASAA2015093013439](https://openairdocs.org/sdr/ASAA2015093013439.md): Stringer Clip · cracked · Sep 30, 2015 · N703AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > STRINGER CLIP AT BS 947 AT 25R IS CRACKED. ACFT GROUNDED. REMOVED, LOCATED AND DRILLED NEW CLIP AND INSTALLED IAW SRM 51-40-02-0G-0, 51-40-05-0G-0.
- [SDR ASAA2015093013453](https://openairdocs.org/sdr/ASAA2015093013453.md): Frame · cracked · Sep 30, 2015 · N703AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME AT BS 400 BETWEEN STRINGERS 8-9L IS CRACKED. ACFT GROUNDED. REPAIRED THE FRAME IAW TC QAD20062609 400-53-107, FIG 2.
- [SDR ASAA2015093013451](https://openairdocs.org/sdr/ASAA2015093013451.md): Angle · cracked · Sep 30, 2015 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 727A AT 25R HAS A CRACKED ATTACH ANGLE. ACFT GROUNDED. REMOVED ANGLE IAW SRM 51-40-02-0G-0, FIG 8 INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0, PARA 4.
- [SDR ASAA2015092913578](https://openairdocs.org/sdr/ASAA2015092913578.md): Spar · corroded · Sep 29, 2015 · N703AS · Boeing 737490 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STABILIZER AFT UPPER ATTACH LUG, STABILIZER SIDE, HAS CORROSION ON AFT FACE. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER AFT UPPER ATTACH LOG CORROSION IAW EA COMPARTMENT 55 EA 15987.
- [SDR ASAA2015092913472](https://openairdocs.org/sdr/ASAA2015092913472.md): Stringer · corroded · Sep 29, 2015 · N703AS · Boeing 737490 · Fuselage Main, Longeron/Stringer
  > STRINGER AT BS 500G AT 27R IS CORRODED AROUND DOMENUT. ACFT GROUNDED. REMOVED CORRODED FROM STR 27R AT BS 500G FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1, FIG 101, DETAIL II, REPAIRED STR 27R AT BS 500G IAW SRM 53-30-03-2R-1, REPAIR 1, W 1.00, O.063, R
- [SDR ASAA2015092913454](https://openairdocs.org/sdr/ASAA2015092913454.md): Attach Angle · cracked · Sep 29, 2015 · N703AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > INTERCOSTAL AT BS 500E AT 26R HAS A CRACKED ATTACHED ANGLE. ACFT GROUNDED. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.
- [SDR ASAA2015092913452](https://openairdocs.org/sdr/ASAA2015092913452.md): Angle · cracked · Sep 29, 2015 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 500E AT 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.
- [SDR ASAA2015092913362](https://openairdocs.org/sdr/ASAA2015092913362.md): Angle · cracked · Sep 29, 2015 · N703AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > INTERCOSTAL AT BS 500F 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.
- [SDR ASAA2015092913361](https://openairdocs.org/sdr/ASAA2015092913361.md): Angle · cracked · Sep 29, 2015 · N703AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > INTERCOSTAL AT BS 500F AT 26R HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PAR 4 AND 7D.
- [SDR ASAA2014081308932](https://openairdocs.org/sdr/ASAA2014081308932.md): Floor Support · cracked · Aug 13, 2014 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT, LBL 24.82 BETWEEN BS 660 - 666 IS CRACKED. ACFT GROUNDED. REPAIRED IAW EA NR AD20080506-400-57-119.
- [SDR ASAA2014081208909](https://openairdocs.org/sdr/ASAA2014081208909.md): Skin · chafed · Aug 12, 2014 · N703AS · Boeing 737490 · Wing Main, Frame Structure
  > LEFT WING INBD EXHAUST GATE UPPER OTBD CORNER IS CHAFED. ACFT GROUNDED. REPAIRED EXHAUST GATE IAW SRM 57-53-01-2R-10 ADJUSTMENT CK GOOD IAW MM 27-51-05-404-016 STEP 3.E5.B-F.
- [SDR ASAA2014081208908](https://openairdocs.org/sdr/ASAA2014081208908.md): Frame · cracked · Aug 12, 2014 · N703AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME BS 360 CRACKED BY A SCREW THAT WAS TOO LONG IN NUT PLATE BETWEEN STRINGERS 12 AND 13L. ACFT GROUNDED. REPAIRED FRAME IAW EA 400, 53EA, 13259.
- [SDR ASAA2014081208899](https://openairdocs.org/sdr/ASAA2014081208899.md): Skin · chafed · Aug 12, 2014 · N703AS · Boeing 737490 · Wing Main, Frame Structure
  > RT WING INDB EXHAUST GATE UPPER SKIN IS CHAFED. ACFT GROUNDED. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR DOUBLER ON RT WING INBD EXHAUST GATE UPPER SKIN IAW SRM 57-53-01-2R-10, REPAIR 10.
- [SDR ASAA2014081208898](https://openairdocs.org/sdr/ASAA2014081208898.md): Skin · chafed · Aug 12, 2014 · N703AS · Boeing 737490 · Trailing Edge Flaps
  > LEFT INBD MID FLAP IS CHAFED AT INBD UPPER EDGE. ACFT GROUNDED. REPAIRED LT INBD MID FLAP INBD UPPER SKIN IAW SRM 57-53-01-2R-3.
- [SDR ASAA2014050907753](https://openairdocs.org/sdr/ASAA2014050907753.md): Light · broken · May 9, 2014 · N703AS · Boeing 737490 · Emergency Lighting
  > AFT OVERWING EXIT DOOR LT SIDE EMERGENCY LIGHT ASSY BROKEN. ACFT GROUNDED. REPLACED AFT LT OVERWING EMERGENCY LIGHT ASSY OPS CHECK GOOD IAW AMM 33-31-01.
- [SDR ASAA2014031007134](https://openairdocs.org/sdr/ASAA2014031007134.md): Lens · dislodged · Mar 10, 2014 · N703AS · Boeing 737490 · Emergency Lighting
  > EXIT LAMP COVER FELL OFF AT RT FORWARD OVERWING EXIT. ACFT GROUNDED. RE-INSTALLED EXIT LENSE COVER RT FWD OVERWING EXIT.
- [SDR ASAA2013061295080](https://openairdocs.org/sdr/ASAA2013061295080.md): Support · cracked · Jun 12, 2013 · N703AS · Boeing 737490 · Wing Miscellaneous Structure
  > NR 6 SLAT ACTUATOR DOOR LANDING ON WING BENT. R & R 36 SLAT ACT DOOR LANDING (SUPPORT) IAW SRM 51-40-02-0G-0.
- [SDR ASAA2013060795016](https://openairdocs.org/sdr/ASAA2013060795016.md): Retainer · cracked · Jun 7, 2013 · N703AS · Boeing 737490 · Wing Miscellaneous Structure
  > SEAL RETAINER CRACKED FOR SEAL ON LWR SHELF PANEL AFT OF RT MLG FOUND DURING SEAL REPLACEMENT. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW RETAINER IAW BDWG 65C35229.
- [SDR ASAA2013060795015](https://openairdocs.org/sdr/ASAA2013060795015.md): Hinge · chafed · Jun 7, 2013 · N703AS · Boeing 737490 · Landing Gear Doors
  > RT MLG OUTER DOOR AFT HINGE ARM CHAFED. ACFTGROUNDED. R & R RT MLG OUTER DOOR AFT HINGE ARM IAW SRM 51-40-02.
- [SDR ASAA2013060795012](https://openairdocs.org/sdr/ASAA2013060795012.md): Retainer · corroded · Jun 7, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > LEFT NR 3 UPPER BLADE SEAL RETAINER IS CORRODED ON BOTTOM SIDE. ACFT GROUNDED. REMOVED CORROSION ON LT NR 3 UPPER BLADE SEAL RETAINER. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW RETAINER IAW SRM 53-60-71-1A-1, FIG 101 AND 51-40-5. NE
- [SDR ASAA2013060795011](https://openairdocs.org/sdr/ASAA2013060795011.md): Retainer · corroded · Jun 7, 2013 · N703AS · Boeing 737490 · Main Landing Gear
  > LT MLG NR 4 LWR BLADE SEAL RETAINER HAS MULTIPLE SPOTS OF CORROSION. ACFT GROUNDED. R & R RETAINER IAW SRM 51-40-05-0G-0, FIG 2, PAGE 5, W.50, O.063, R.056, L 8.0, D 0.007.
- [SDR ASAA2013060795010](https://openairdocs.org/sdr/ASAA2013060795010.md): Fairing · chafed · Jun 7, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > RIGHT AFT NR 5 MLG SKI JUMP FAIRING IS CHAFED. ACFT GROUNDED.
- [SDR ASAA2013060795009](https://openairdocs.org/sdr/ASAA2013060795009.md): Support Bracket · cracked · Jun 7, 2013 · N703AS · Boeing 737490 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENG PYLON AFT RT PANEL SUPPORT BRACKET CRACKED ON UPPER END (AFT OF RT MID SPAR ATTACH PIN LUG) ACFT GROUNDED. REMOVED NR 2 OTBD SUPPORT ASSY, FABRICATED NEW ANGLE INSTALLED SUPPORT ASSY IAW SRM 51-40-02 AND 51-40-05-0G 0.
- [SDR ASAA2013060795008](https://openairdocs.org/sdr/ASAA2013060795008.md): Web · gouged · Jun 7, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT LWR FWD REVEAL WEB IS DAMAGED ALONG AFT EDGE. ACFT GROUNDED. FABRICATED NEW REVEAL IAW SRM 51-70-13, OG 0 AND DWG NO 65-56655-2.
- [SDR ASAA2013060695022](https://openairdocs.org/sdr/ASAA2013060695022.md): Skin · dented · Jun 6, 2013 · N703AS · Boeing 737490 · Trailing Edge Flaps
  > RT INBD FOREFLAP FOUND DENT CLUSTER ON LWR SURFACE STARTING AT 43" FROM INBD END TO 53" AND 2 TO 12" FROM T/E. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2013060395052](https://openairdocs.org/sdr/ASAA2013060395052.md): Tab · damaged · Jun 3, 2013 · N703AS · Boeing 737490 · Elevator, Tab Structure
  > LEFT ELEVATOR TAB INBD EDGE IS DAMAGED. BONDED REPAIR ON LT ELEVATOR TAB, INBD CORNER EDGE IAW SRM 51-70-17, REPAIR 11.
- [SDR ASAA2013053194994](https://openairdocs.org/sdr/ASAA2013053194994.md): Seat · cracked · May 31, 2013 · N703AS · Boeing 737490 · Passenger/Crew Doors
  > L1 DOOR FWD UPPER DOOR SEAL LOCATOR IS CRACKED. R & R L1 DOOR FWD SEAL LOCATOR IAW BAC5065, PG 24-27.
- [SDR ASAA2013053194968](https://openairdocs.org/sdr/ASAA2013053194968.md): Skin · dented · May 31, 2013 · N703AS · Boeing 737490 · Spoilers
  > NR 3 SPOILER UPPER SURFACE DENTED WITH A CREASE LOCATION 4.5 FROM T/E AND 12 FROM INBD END. REPAIRED NR 3 SPOILER UPPER AFT INBD SKIN IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2013052895002](https://openairdocs.org/sdr/ASAA2013052895002.md): Structure · corroded · May 28, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > RIGHT WHEEL WELL MANIFOLD ASSY LOWER FWD STRUCTURE HAS BARE METAL AND SURFACE CORRODED, FWD AND AFT SIDES. ACFT GROUNDED. BLENDED CORROSION, FOUND TO BE 100 MATERIAL LOSS IAW SRM 53-60-71. FABRICATED NEW LOWER FWD STRUCTURE IAW SRM 51-40-02. INSTALLED NEW
- [SDR ASAA2013052894883](https://openairdocs.org/sdr/ASAA2013052894883.md): Skin · dented · May 28, 2013 · N703AS · Boeing 737490 · Fuselage Main, Plate/Skin
  > FUSELAGE DAMAGE AFT OF L2 DOOR BOTTOM CORNER. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AFT OF L2 DOOR BOTTOM CORNER STA 1010, STR 15L IAW SRM 53-00-01-2R-35.
- [SDR ASAA2013052694983](https://openairdocs.org/sdr/ASAA2013052694983.md): Strap · cracked · May 26, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT UNDER STRAP, FS 847-867 IS CRACKED. ACFT GROUNDED. FABRICATED NEW STRAP STA 847-867, STR 25R IAW SRM 51-40-05-0G-0 STRAP TO BE INSTALLED ON MIG5 5408009.
- [SDR ASAA2013052694885](https://openairdocs.org/sdr/ASAA2013052694885.md): Floorbeam · corroded · May 26, 2013 · N703AS · Boeing 737490 · Fuselage Main, Floor Beam
  > ON REMOVAL OF NR 2 AFT CARGO FLOORBOARD, FOUND FLOOR SPLICE AT BS 727D CORRODED. ACFT GROUNDED. BLENDED AND FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRIMED AND TOPCOATED NEW FLOORBOARD SPLICE IAW SRM 53-60-53, FIG 101-51-10-02-0G-0, 51-40 05-00-0 AN
- [SDR ASAA2013052495004](https://openairdocs.org/sdr/ASAA2013052495004.md): Door Frame · corroded · May 24, 2013 · N703AS · Boeing 737490 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT FWD FRAME REPAIR DOUBLER IS CORRODED. FOUND ON REMOVAL OF TRANSITION PANEL. ACFT GROUNDED. R & R AFT CARGO DOOR CUTOUT FWD FRAME AND FACTORY DOUBLER IAW SRM 51-40-02.
- [SDR ASAA2013052295048](https://openairdocs.org/sdr/ASAA2013052295048.md): Stiffener · corroded · May 22, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > APU BAY RT TORQUE BOX INLET CUTOUT LOWER STIFFENER IS CORRODED, BS 1118-1127. R & R RT TORQUE BOX INLET CUTOUT LOWER STIFFENER IAW SRM 51-40-05-0G-0 AND 51-40-02-0G-0.
- [SDR ASAA2013052295013](https://openairdocs.org/sdr/ASAA2013052295013.md): Retainer · corroded · May 22, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > LEFT MLG NR 3 LOWER BLADE SEAL RETAINER HAS BARE METAL. ACFT GROUNDED. R & R LEFT MLG NR 3 LWR BLADE SEAL RETAINER IAW SRM 51-40-05-0G-0, FIG 2, PAGE 5, W 0.50, O 0.063, R 0.054, L 4.0, D 0.009.
- [SDR ASAA2013052294880](https://openairdocs.org/sdr/ASAA2013052294880.md): Stiffener · corroded · May 22, 2013 · N703AS · Boeing 737490 · APU Cowling/Containment
  > APU COMPARTMENT RT TORQUE BOX INLET CUTOUT UPPER STIFFENER IS CORRODED STA 1112 TO 1127. ACFT GROUNDED. R & R TORQUE BOX CUT OUT UPPER STIFFENER IAW SRM 51-40-02-0G-0.
- [SDR ASAA2013052195014](https://openairdocs.org/sdr/ASAA2013052195014.md): Web · corroded · May 21, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF AFT RT LWR MANIFOLD STRUCTURE FOUND WEB TO BE CORRODED. ACFT GROUNDED. REPAIRED RT MLG MANIFOLD WEB IAW EA 400 53, EA 10436, REV NEW DATED 30MAY13.
- [SDR ASAA2013052095001](https://openairdocs.org/sdr/ASAA2013052095001.md): Support Angle · cracked · May 20, 2013 · N703AS · Boeing 737490 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON INBD AFT SUPPORT ANGLE AFT OF FUSE PIN IS CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED NR 1 PYLON INBD SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR ASAA2013052094916](https://openairdocs.org/sdr/ASAA2013052094916.md): Web · cracked · May 20, 2013 · N703AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > L1 AFT REVEAL WEB IS CRACKED. FABRICATED NEW WEB L1 AFT REVEAL IAW BAC DWG 65-17685.
- [SDR ASAA2013051915373](https://openairdocs.org/sdr/ASAA2013051915373.md): Floor Panel · corroded · May 19, 2013 · N703AS · Boeing 737490 · Fuselage Floor Panel
  > UPON REMOVAL OF PIT SIDEWALL PANEL FOUND NR 1 FLOOR PANEL RT EDGE TO HAVE LIGHT SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION ON NR 1 FLOOR PANEL MATERIAL LOSS FOUND TO BE OUT OF LIMITS AND FABRICATED NEW FLOOR PANEL IAW SRMS 53-60-53-1A-1 AND 51-40-05-
- [SDR ASAA2013051995018](https://openairdocs.org/sdr/ASAA2013051995018.md): Angle · chafed · May 19, 2013 · N703AS · Boeing 737490 · Wing Miscellaneous Structure
  > LT WING INBD UPPER T/E SHELF PANEL ATTACH ANGLE CHAFED ON LWR SIDE. ACFT GROUNDED. DAMAGE AREA FOUND TO BE OUT OF LIMITS IAW SRM 57-51-02-1A-1. R & R ANGLE IAW SRM 51-40-02-0G-0.

Next page: https://openairdocs.org/deregistered/N703AS-2018-11-28/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 = 'N703AS' AND deregistration_id = 'N703AS-2018-11-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N703AS-2018-11-28/reports

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