# Service difficulty reports: N796AS, cancelled Sep 15, 2016

A list on [N796AS, cancelled Sep 15, 2016](https://openairdocs.org/deregistered/N796AS-2016-09-15.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 4 · 186 reports

- [SDR ASAA2016041216372](https://openairdocs.org/sdr/ASAA2016041216372.md): Lens · detached · Apr 12, 2016 · N796AS · Boeing 737490 · Emergency Lighting
  > EMERGENCY LIGHT AT 16DEF PUSHED IN. ACFT GROUNDED. RE-INSTALLED LIGHT AT 16DEF, OPS CHECKS GOOD.
- [SDR ASAA2016021415438](https://openairdocs.org/sdr/ASAA2016021415438.md): Lens · detached · Feb 14, 2016 · N796AS · Boeing 737490 · Emergency Lighting
  > EXIT SIGN FELL OFF EMERGENCY EXIT ROW LT SIDE. ACFT GROUNDED. REINSTALLED EXIT SIGN LENS, NO DAMAGE NOTED. EMERGENCY EXIT LIGHT OPS CK GOOD REF AMM 33-51-11.
- [SDR ASAA2016010414644](https://openairdocs.org/sdr/ASAA2016010414644.md): Lamp · inoperative · Jan 4, 2016 · N796AS · Boeing 737490 · Emergency Lighting
  > EMERGENCY LIGHT EXIT SIGN ABOVE L-2 DOOR HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-11-962-002. OPS NORMAL.
- [SDR ASAA2015102813576](https://openairdocs.org/sdr/ASAA2015102813576.md): Skin · damaged · Oct 28, 2015 · N796AS · Boeing 737490 · Fuselage Main, Plate/Skin
  > RIGHT NOSE GEAR DOOR AND ADJACENT STRUCTURE DAMAGED. ACFT GROUNDED. INSTALLED REPAIR DOUBLER TO DAMAGED FUSELAGE SKIN AND REPLACED GEAR DOOR.
- [SDR ASAA2015100113439](https://openairdocs.org/sdr/ASAA2015100113439.md): Attach Angle · cracked · Oct 1, 2015 · N796AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > INTERCOSTAL ATTACH ANGLE AT BS 348.2 STR 15L IS CRACKED. ACFT GROUNDED. REPAIRED IAW AD20121205-400-53-2.
- [SDR ASAA2015092913438](https://openairdocs.org/sdr/ASAA2015092913438.md): Beam · cracked · Sep 29, 2015 · N796AS · Boeing 737490 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD END E BEAM OUTER ANGLE IS CRACKED AT 3RD FASTENER AFT VERTICAL LEG. ACFT GROUNDED. REPAIRED AFT CARGO DOOR FWD END E BEAM OUTER ANGLE IAW T/C AD20131312-400-52-15, REV 00, DATED 18AUG14 AND DWG 65C37547.
- [SDR ASAA2015012811114](https://openairdocs.org/sdr/ASAA2015012811114.md): Housing · gouged · Jan 28, 2015 · N796AS · Boeing 737490 · Cargo/Baggage Doors
  > AFT CARGO DOOR HANDLE HOUSING GOUGED FROM HANDLE DUE TO MISSING BUMPER. ACFT GROUNDED. REMOVED THE INTERIOR AND EXTERIOR DOOR HANDLES FROM THE AFT CARGO DOOR REF AMM 52-31-14. R & R PAN HOUSING REF SRM 51-40-02 SEALED HOUSING AND RIVETED. INSTALLED DOOR HAN
- [SDR ASAA2014121410062](https://openairdocs.org/sdr/ASAA2014121410062.md): Seal Depressor · cracked · Dec 14, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF FAIRING COMPOUND, FOUND R2 DOOR LOWER HINE SEAL DEPRESSOR FITTING CRACKED. ACFT GROUNDED. REMOVED DAMAGED LOWER SEAL DEPRESSOR FITTING AND INSTALLED A NEW ONE AT THE FWD LOWER FRAME AT THE R2 DOOR IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014121410061](https://openairdocs.org/sdr/ASAA2014121410061.md): Seal Depressor · corroded · Dec 14, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF FAIRING COMPOUND, FOUND L2 DOOR LOWER HINGE SEAL DEPRESSOR CORRODED. ACFT GROUNDED. R & R IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, W 1, O.080, R 0, L 1, D.080.
- [SDR ASAA2014121409964](https://openairdocs.org/sdr/ASAA2014121409964.md): Fitting · cracked · Dec 14, 2014 · N796AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > AFTER REMOVAL OF FAIRING COMPOUND FOUND L2 DOOR UPPER HINGE SEAL DEPRESSOR FITTING CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, FIG 2.
- [SDR ASAA2014121409962](https://openairdocs.org/sdr/ASAA2014121409962.md): Fitting · cracked · Dec 14, 2014 · N796AS · Boeing 737490 · Fuselage Main, Attach Fittings
  > AFTER REMOVAL OF FAIRING COMPOUND FOUND R2 DOOR HINGE UPPER SEAL DEPRESSOR FITTING CRACKED. ACFT GROUNDED. REMOVED CRACKED UPPER SEAL DEPRESSOR FITTING AND INSTALLED A NEW SEAL DEPRESSOR FITTING ON FWD FRAME OF R2 DOOR IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014101909433](https://openairdocs.org/sdr/ASAA2014101909433.md): Lens · detached · Oct 19, 2014 · N796AS · Boeing 737490 · Emergency Lighting
  > F/A REPORTS ROW 16DEF EMERGENCY EXIT SIGN FALLING DOWN ON OVERWING EXIT. ACFT GROUNDED. SECURED EXIT SIGN ABOVE SEAT 16F. NO DEFECTS NOTED.
- [SDR ASAA2014070808641](https://openairdocs.org/sdr/ASAA2014070808641.md): Stiffener · corroded · Jul 8, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > APU BAY RT TORQUE BOX AIR INLET CUT OUT, AFT STIFFENER CORRODED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014070708621](https://openairdocs.org/sdr/ASAA2014070708621.md): Angle · cracked · Jul 7, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT BS 294.5 BETWEEN S9-10R. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02, INSTALLED FABRICATED ANGLE STIFFENER IAW SRM 51-40-02.
- [SDR ASAA2014070708620](https://openairdocs.org/sdr/ASAA2014070708620.md): Angle · cracked · Jul 7, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT FS 294.5 BETWEEN STR 12-13 RT. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02 LOCATED AND DRILLED NEW ANGLE STIFFENER IAW SRM 51-40-05, INSTALLED IAW SRM 51-40-02.
- [SDR ASAA2014070708619](https://openairdocs.org/sdr/ASAA2014070708619.md): Angle · cracked · Jul 7, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT BS 294.5 BETWEEN STR 11-12 RT. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-40-05 AND SRM 51-40-02.
- [SDR ASAA2014070308816](https://openairdocs.org/sdr/ASAA2014070308816.md): Frame · cracked · Jul 3, 2014 · N796AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME BS 787, CRACKED BETWEEN STRINGERS 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.
- [SDR ASAA2014070308814](https://openairdocs.org/sdr/ASAA2014070308814.md): Frame · cracked · Jul 3, 2014 · N796AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME BS 500A CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.
- [SDR ASAA2014070308813](https://openairdocs.org/sdr/ASAA2014070308813.md): Frame · cracked · Jul 3, 2014 · N796AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME BS 907 CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.
- [SDR ASAA2014070308812](https://openairdocs.org/sdr/ASAA2014070308812.md): Frame · cracked · Jul 3, 2014 · N796AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME BS 727D CRACKED BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.
- [SDR ASAA2014070308811](https://openairdocs.org/sdr/ASAA2014070308811.md): Frame · cracked · Jul 3, 2014 · N796AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME BS 727D CRACKED BETWEEN STRINGERS 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609 400-53-132, REV.
- [SDR ASAA2014070308655](https://openairdocs.org/sdr/ASAA2014070308655.md): Frame · cracked · Jul 3, 2014 · N796AS · Boeing 737490 · Fuselage Main, Frame
  > FRAME AT BS 480 HAS A CRACK BETWEEN STRINGERS 8-9R. ACFT GROUNDED. REPAIRED FRAME IAW ASA EA AD20062609 400-53-132, REV NEW DATED.
- [SDR ASAA2014070215159](https://openairdocs.org/sdr/ASAA2014070215159.md): Floor Support · corroded · Jul 2, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT, LBL 10, BS 328 - 344 HAS CORROSION. ACFT GROUNDED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014070208817](https://openairdocs.org/sdr/ASAA2014070208817.md): Channel · corroded · Jul 2, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > L1 DOOR MOPSILL HAS MULTIPLE AREAS OF CORROSION. ACFT GROUNDED. R & R MOPSILL, IAW EA 400-53EA-13151.
- [SDR ASAA2014070208774](https://openairdocs.org/sdr/ASAA2014070208774.md): Floorbeam · corroded · Jul 2, 2014 · N796AS · Boeing 737490 · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER CAP FROM LBL 39-RBL 45 IS CORRODED IN SEVERAL AREAS. ACFT GROUNDED. BLENDED DAMAGE IAW SRM 53-60-51-1A-1. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-60-51-1A-1. REPAIRED DAMAGED TEE IAW EA 400-53EA-13131, REV NEW.
- [SDR ASAA2014070208708](https://openairdocs.org/sdr/ASAA2014070208708.md): Floorbeam · corroded · Jul 2, 2014 · N796AS · Boeing 737490 · Fuselage Main, Floor Beam
  > BS 344 FLOORBEAM HAS A SPOT OF CORROSION ON UPPER CAP AT LBL 10. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS AND REPAIRED IAW EA 400, 53EA 13112.
- [SDR ASAA2014070208667](https://openairdocs.org/sdr/ASAA2014070208667.md): Skin · chafed · Jul 2, 2014 · N796AS · Boeing 737490 · Leading Edge Devices
  > LT INBD FOREFLAP UPPER SURFACE CHAFED AT PREVIOUS REPAIR. ACFT GROUNDED. REPAIRED LT INBD FOREFLAP UPPER SURFACE AT PREVIOUS REPAIR IAW SRM 51-20-10-2R-0, REPAIR 4.
- [SDR ASAA2014070208658](https://openairdocs.org/sdr/ASAA2014070208658.md): Channel · corroded · Jul 2, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > L2 DOOR MOP SILL HAS CORROSION AT FWD END OF DOORWAY. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A-1. R & R MOP SILL IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014070208656](https://openairdocs.org/sdr/ASAA2014070208656.md): Floor Support · corroded · Jul 2, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FWD FLOOR SUPPORT, LBL 10, BS 328-344 CORRODED. ACFT GROUNDED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014070208618](https://openairdocs.org/sdr/ASAA2014070208618.md): Intercostal · cracked · Jul 2, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FWD WET INTERCOSTAL, LBL 45, BS 312-328 IS CRACKED AT FASTENER HOLE ON UPPER SURFACE. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR ASAA2014070108815](https://openairdocs.org/sdr/ASAA2014070108815.md): Skin · delaminated · Jul 1, 2014 · N796AS · Boeing 737490 · Trailing Edge Flaps
  > LEFT OTBD AFT FLAP OTBD CORNER DELAMINATED. ACFT GROUNDED. REPAIRED LT OTBD AFT FLAP OTBD CORNER IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2014070108659](https://openairdocs.org/sdr/ASAA2014070108659.md): Floorbeam · corroded · Jul 1, 2014 · N796AS · Boeing 737490 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOORBEAM TEE SPLICE BETWEEN NR 1 AND 2 FLOOR PANELS HAS MULTIPLE AREAS OF CORRODED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE IAW SRM 53-60-53-1A-1, & 51-40-05-0G-0.
- [SDR ASAA2014070108622](https://openairdocs.org/sdr/ASAA2014070108622.md): Skin · delaminated · Jul 1, 2014 · N796AS · Boeing 737490 · Trailing Edge Flaps
  > LEFT OTBD AFT FLAP OTBD CORNER DELAMINATED. ACFT GROUNDED. REPAIRED LT OTBD AFT FLAP OTBD CORNER IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2014070108584](https://openairdocs.org/sdr/ASAA2014070108584.md): Support · corroded · Jul 1, 2014 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > FWD CARGO LT TRANSITION IS CORRODED AT STA 500G. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS SRM 53-30-53-1A-1 FABRICATED NEW TRANSITION PANEL IAW 400 SRM 51-40-05-0G-0, 51-20-01-0G-0, SOPM 20-41-02 AND SRM 51-40-02-0G-0, AND SRM 53-30-53-2R-3.
- [SDR ASAA2013101708669](https://openairdocs.org/sdr/ASAA2013101708669.md): Skin · cracked · Oct 17, 2013 · N796AS · Boeing 737490 · Leading Edge Devices
  > NR 2 L/E SLAT LOWER T/E HAS POSSIBLE CRACK AT RIVET HEAD, MARKED. ACFT GROUNDED. REPAIRED NR 2 L/E SLAT LOWER T/E SKIN IAW SRM 57-43-01-2R-6.
- [SDR ASAA2013033194328](https://openairdocs.org/sdr/ASAA2013033194328.md): Threshold · corroded · Mar 31, 2013 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > LEFT AFT LAVATORY THRESHOLD AFT HAS BULGED AREA ON AFT SIDE. REPAIRED AFT LAVATORY THRESHOLD BULGING AREA IAW NA 25-46-99, REPAIR 2 & 4 AND EA 400-25EA-10035.
- [SDR ASAA2013031994331](https://openairdocs.org/sdr/ASAA2013031994331.md): Skin · chafed · Mar 19, 2013 · N796AS · Boeing 737490 · Leading Edge Devices
  > RT OTBD FORE FLAP PREVIOUS REPAIR ON OTBD L/E CHAFED. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-53-01, FIG 201.
- [SDR ASAA2013031994282](https://openairdocs.org/sdr/ASAA2013031994282.md): Skin · deformed · Mar 19, 2013 · N796AS · Boeing 737490 · Fuselage Main, Plate/Skin
  > LEFT FUSELAGE SKIN IS DENTED FWD OF THE ALTERNATE STATIC PORT. REPAIRED IAW EA 400-53, EA 10047.
- [SDR ASAA2013031894330](https://openairdocs.org/sdr/ASAA2013031894330.md): Floor Panel · corroded · Mar 18, 2013 · N796AS · Boeing 737490 · Fuselage Floor Panel
  > AFT CARGO BAY BS 945 AFT FLOOR PANEL HAS CORROSION ON AFT RT END. REMOVED, FABRICATED NEW AND INSTALLED NEW FLOOR PANEL IAW AMM 25-52-51-004-001, PARA C, 25-52-51-404-011 PARA D, SRM 51-40-05, FIG 2, DETAIL I, 51-20-01 PARA G AND SOPM 20-41-02, PARA 6F. FOUN
- [SDR ASAA2013031894261](https://openairdocs.org/sdr/ASAA2013031894261.md): Wedge · chafed · Mar 18, 2013 · N796AS · Boeing 737490 · Leading Edge Devices
  > RT WING NR 4 SLAT INBD T/E WEDGE LOWER SURFACE IS CHAFED. REPAIRED RT WING NR 4 SLAT INBD T/E WEDGE LOWER SURFACE IAW SRM 51 70 10, REPAIR 4.
- [SDR ASAA2013031894229](https://openairdocs.org/sdr/ASAA2013031894229.md): Floor Panel · corroded · Mar 18, 2013 · N796AS · Boeing 737490 · Fuselage Floor Panel
  > AFT CARGO NR 2 FLOOR PANEL HAS CORROSION. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05, FIG 2, DETAIL I, 51 20 01 PARA 6 AND SOPM 20 41 02, PARA 6.F. REMOVED CORRODED ON NR 2 FLOOR PANEL AND FOUND TO BE OUT OF LIMITS IAW SRM 53 60 53, FIG 19 DETAIL V.
- [SDR ASAA2013031894227](https://openairdocs.org/sdr/ASAA2013031894227.md): Skin · dented · Mar 18, 2013 · N796AS · Boeing 737490 · Trailing Edge Flaps
  > LEFT OTBD FOREFLAP L/E IS DENTED APPORX 6 FROM INBD. REMOVED, FABRICATED AND INSTALLED NEW L/E SKIN IAW SRM 51 40 05, 51 40 02.
- [SDR ASAA2013031894225](https://openairdocs.org/sdr/ASAA2013031894225.md): Wedge · chafed · Mar 18, 2013 · N796AS · Boeing 737490 · Leading Edge Devices
  > RT WING NR 5 SLAT INBD T/E WEDGE LOWER SURFACE IS CHAFED ON A PREVIOUS REPAIR. REPAIRED RT WING NR 5 SLAT INBD T/E WEDGE LOWER SURFACE IAW SRM 51 70 10, REPAIR 4.
- [SDR ASAA2012111793363](https://openairdocs.org/sdr/ASAA2012111793363.md): Floor Panel · punctured · Nov 17, 2012 · N796AS · Boeing 737490 · Fuselage Floor Panel
  > REPORTED HOLE IN FLOOR PANEL, AFT CARGO BAY FS 727E. REMOVED DAMAGED AREA AND SECURED DOUBLER IAW SRM 53-60-53 REPAIR 6 AND SRM 51-70-13.
- [SDR ASAA11410159](https://openairdocs.org/sdr/ASAA11410159.md): Engine · surges · Jul 23, 2011 · N796AS · Boeing 737490 · Engine (Turbine/Turboprop)
  > ALMOST TO TOP OF CLIMB (18 MIN INTO FLIGHT) BOTH PILOTS HEARD AN ENGINE SURGE NR 1 N1 99% NR 2 N1 96%. NR 1 N1 CAME RIGHT DOWN TO 96%. ON APPROACH HAD A ONE THROTTLE KNOB WIDTH TO MATCH POWER (31 ENGINE THROTTLE BACK TO MATCH) SURGE WAS VERY NOTICABLE IN PAX
- [SDR ASAA0946371](https://openairdocs.org/sdr/ASAA0946371.md): Beam · corroded · Aug 7, 2009 · N796AS · Boeing 737490 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO TIE DOWN BEAM HAS MULTIPLE AREAS OF CORROSION FROM STA 778 TO 860 ALONG STR 26R. REPAIRED AFT CARGO TIE DOWN.
- [SDR ASAA0946364](https://openairdocs.org/sdr/ASAA0946364.md): Fitting · gouged · Aug 6, 2009 · N796AS · Boeing 737490 · Fuselage Main, Longeron/Stringer
  > UPON BOLT REPLACEMENT FOUND STR END FITTING STR 10L AFT SIDE STA 1016 LOWER HOLE GOUGED. REMOVED AND REPLACED STR 10L FWD END FITTING IAW SRM.
- [SDR ASAA0946363](https://openairdocs.org/sdr/ASAA0946363.md): Floor Support · corroded · Aug 6, 2009 · N796AS · Boeing 737490 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT ANGLE STA 793 AND STR 27R CORRODED AT SPLICE. REPAIRED AFT CARGO FLOOR SUPPORT ANGLE IAW ASA EA.
- [SDR ASAA0946362](https://openairdocs.org/sdr/ASAA0946362.md): Floorbeam · corroded · Aug 6, 2009 · N796AS · Boeing 737490 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CORRODED LBL 43 LBL 26 STA 986. REPAIRED FLOORBEAM BETWEEN RBL 20 LBL 57.
- [SDR ASAA0946361](https://openairdocs.org/sdr/ASAA0946361.md): Fitting · damaged · Aug 6, 2009 · N796AS · Boeing 737490 · Fuselage Main, Longeron/Stringer
  > UPON BOLT REPLACEMENT FOUND STR END FITTING STR 10L AFT SIDE STA 1016 LOWER HOLE ELONGATED. REMOVED AND REPLACED STR 10L AFT END FITTING IAW SRM.

Next page: https://openairdocs.org/deregistered/N796AS-2016-09-15/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 = 'N796AS' AND deregistration_id = 'N796AS-2016-09-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N796AS-2016-09-15/reports

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