# Service difficulty reports: N778AS, cancelled Feb 13, 2017

A list on [N778AS, cancelled Feb 13, 2017](https://openairdocs.org/deregistered/N778AS-2017-02-13.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 8 · 362 reports

- [SDR ASAA2016051916948](https://openairdocs.org/sdr/ASAA2016051916948.md): Frame · dented · May 19, 2016 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > DENT ON FRAME AT BS 1121 LBL 25 WL 285. ACFT GROUNDED. REPAIRED FRAME AT BS 1121, LBL 25, WL 285 IAW SRM 51-70-11.
- [SDR ASAA2016050416628](https://openairdocs.org/sdr/ASAA2016050416628.md): Strap · cracked · May 4, 2016 · N778AS · Boeing 7374Q8 · Fuselage Main, Floor Beam
  > FOUND LT OTBD FLOORBEAM STRAP CRACKED AT BS 312, LBL 12. ACFT GROUNDED. R & R FLOORBEAM STRAP IAW DWG 65-45834 AND SRM 51-40-02.
- [SDR ASAA2016012114974](https://openairdocs.org/sdr/ASAA2016012114974.md): Arm · loose · Jan 21, 2016 · N778AS · Boeing 7374Q8 · Passenger/Crew Doors
  > F/A REPORTED L-1 DOOR VERY DIFFICULT TO CLOSE. ACFT GROUNDED. INSPECTED L-1 DOOR FOUND JAM NUT ON GUIDE ARM LOOSE READJUSTED GUIDE ARM AS REQUIRED TIGHTENED JAM NUT AND SECURED SECONDARY COVER, REF MM 52-11-00. OPS CHECK OF L-1 DOOR IS GOOD.
- [SDR ASAA2016011314772](https://openairdocs.org/sdr/ASAA2016011314772.md): Lamp · inoperative · Jan 13, 2016 · N778AS · Boeing 7374Q8 · Emergency Lighting
  > L-1 DOOR EMERGENCY EXIT IDENTIFIER LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS, OPS CHECKED NORMAL.
- [SDR ASAA2016011314771](https://openairdocs.org/sdr/ASAA2016011314771.md): Battery Pack · failed · Jan 13, 2016 · N778AS · Boeing 7374Q8 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1132, EXTINGUISH AFTER 1 MINUTE OF OPERATION. ACFT GROUNDED. REPLACED PACK BATTERY PACK. OPS CK NORMAL.
- [SDR ASAA2015040211409](https://openairdocs.org/sdr/ASAA2015040211409.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME BS 867, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3 REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211408](https://openairdocs.org/sdr/ASAA2015040211408.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME AT STA 867 HAS CRACK AT INBD FASTENER BETWEEN S8L & S9L ACFT BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 867 LT IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3, REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211407](https://openairdocs.org/sdr/ASAA2015040211407.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME 440 CRACK AT INBD BRACKET FASTENER TO RADIUS. ACFT GROUNDED. REPAIRED FRAME IAW 10 292077 TASKCARD AD 200 62-6009-400-53-1, REV 01, REV DATE 03, 30, 2015, FIG 3. REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211406](https://openairdocs.org/sdr/ASAA2015040211406.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME AT BS 480 HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L, AC BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 480L IAW W/O 292077 TASKCARD AD 20062 609-400-53-01, REV 01, REV DATE 03/30/2015, FIG 3. REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211405](https://openairdocs.org/sdr/ASAA2015040211405.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME BS 907R, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME 907R IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3 REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211404](https://openairdocs.org/sdr/ASAA2015040211404.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME BS 500A RT CRACK AT INBD BRACKET FASTENER FRAME. ACFT GROUNDED. REPAIRED FRAME 500A IAW W/O 292077, T/C AD 2002609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3, REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211403](https://openairdocs.org/sdr/ASAA2015040211403.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME BS 907, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME 907R IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3, REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211401](https://openairdocs.org/sdr/ASAA2015040211401.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME BS 727F, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW W/O 292077 TASK CARD AD20062609-400-53-1, REV 01, REV DATE 03/30/2015, FIG 3. REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211399](https://openairdocs.org/sdr/ASAA2015040211399.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME AT BS 400L HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW WO 292077 TASK CARD AD 20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211398](https://openairdocs.org/sdr/ASAA2015040211398.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME AT BS 500A CRACKED AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 500A LT IAW ASA WO 292077 TASK CARD, AD 20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211397](https://openairdocs.org/sdr/ASAA2015040211397.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME 827R, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW WO 292077 TASK CARD AD20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211396](https://openairdocs.org/sdr/ASAA2015040211396.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME AT BS 500C CRACKED AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 500C LT IAW W/O 292077, TASK CARD AD20062609-400-53-1, REV 01, REV DATE 03/30/2015, FIG 3.
- [SDR ASAA2015040211395](https://openairdocs.org/sdr/ASAA2015040211395.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME AT BS 727B HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 727B LT IAW ASA WO 292077, TASK CARD AD 20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.
- [SDR ASAA2015040211394](https://openairdocs.org/sdr/ASAA2015040211394.md): Frame · cracked · Apr 2, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Frame
  > FRAME AT BS 440L HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L A/C BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW AD 20062609-400-53-1, REV 01, REV.
- [SDR ASAA2015040111410](https://openairdocs.org/sdr/ASAA2015040111410.md): Spar · corroded · Apr 1, 2015 · N778AS · Boeing 7374Q8 · Horizontal Stabilizer, Spar/Rib
  > LT HORIZONTAL STABILIZER ATTACH FITTING UPPER LUG CORRODED AROUND BUSHING. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER FRONT SPAR UPPER TERMINAL FITTING LUG AND JOINT IAW EAC MPT-55EA-14908 IAW ASSOCIATED FORM 8100-9. THIS IS A CATEGORY B REPAIR FIRST ST
- [SDR ASAA2015033111402](https://openairdocs.org/sdr/ASAA2015033111402.md): Attach Angle · cracked · Mar 31, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Attach Fittings
  > INTERCOSTAL ATTACH ANGLE CRACKED AT BS 348 AND STR 15L. ACFT GROUNDED. R & R CLIP ANGLE IAW TASK CARD AD20121205-400-53-2, STEP 9, 10, 11. REF TASK CARD: AD20121205-400-53-4A.
- [SDR ASAA2015033111400](https://openairdocs.org/sdr/ASAA2015033111400.md): Attach Angle · cracked · Mar 31, 2015 · N778AS · Boeing 7374Q8 · Fuselage Main, Attach Fittings
  > INTERCOSTAL ATTACH ANGLE CRACKED AT BS 348 AND STR 16 LT. ACFT GROUNDED. R & R INTERCOSTAL WEB, ATTACH ANGLE IAW TC AD20121205-400-53-2, STEP 15, 16, 17. REF TASK CARD: AD20121205-400-53-4A.
- [SDR ASAA2015011110228](https://openairdocs.org/sdr/ASAA2015011110228.md): Battery Pack · failed · Jan 11, 2015 · N778AS · Boeing 7374Q8 · Emergency Lighting
  > WHILE PERFORMING INTERIOR EMERGENCY LIGHT CHECK. FOUND INTERIOR EMERGENCY LIGHT ROW 25 LEFT INOPERATIVE. ALSO, FOUND LT AFT OFF WING EXTERIOR LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP IAW AMM 33-55-00. OPS CHECK NO GOOD. R & R M1576 BATTERY CHA
- [SDR ASAA2015011110227](https://openairdocs.org/sdr/ASAA2015011110227.md): Reflector · failed · Jan 11, 2015 · N778AS · Boeing 7374Q8 · Emergency Lighting
  > DURING EMERGENCY LIGHT CK FOUND RT FWD EXTERIOR LIGHT INOPERATIVE AFT OF THE R1 DOOR. ACFT GROUNDED. REPLACED LIGHT REFLECTOR IAW CMM 33-50-27, OPS CHECK GOOD.
- [SDR ASAA2014010512304](https://openairdocs.org/sdr/ASAA2014010512304.md): Skin · cracked · Jan 5, 2014 · N778AS · Boeing 7374Q8 · Wing, Plate/Skin
  > NR 3 L/E SLAT ACTUATOR CUTOUT CRACKED. ACFT GROUNDED. REPAIRED NR 3 L/E SLAT ACTUATOR CUTOUT IAW SRM 57-41-01-2R-7, REPAIR 4, PROCEDURE 1.
- [SDR ASAA2013121812307](https://openairdocs.org/sdr/ASAA2013121812307.md): Web · damaged · Dec 18, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > SHEAR WEB AFT OF L1 DOOR IS DAMAGED. ACFT GROUNDED. DISSASSEMBLED SHEAR WEB AFT OF L2 DOOR, FABBED NEW WEB, RE-ASSEMBLED SHEAR WEB IAW SRM 51-40-02-0G-0, 4-51-30-01-0G-0, NR 8.
- [SDR ASAA2013121812239](https://openairdocs.org/sdr/ASAA2013121812239.md): Skin · chafed · Dec 18, 2013 · N778AS · Boeing 7374Q8 · Trailing Edge Flaps
  > RIGHT OTBD MID FLAP OTBD L/E CORNER IS CHAFED. REPAIRED RT OTBD MID FLAP OTBD L/E CORNER IAW SRM 57-53-01-2R-8.
- [SDR ASAA2013121812238](https://openairdocs.org/sdr/ASAA2013121812238.md): Skin · chafed · Dec 18, 2013 · N778AS · Boeing 7374Q8 · Trailing Edge Flaps
  > LEFT WING OTBD MIDFLAP INBD L/E IS CHAFED. REPAIRED LT OTBD MIDFLAP INBD L/E IAW SRM 57-53-01-2R-8.
- [SDR ASAA2013121612301](https://openairdocs.org/sdr/ASAA2013121612301.md): Attach Angle · corroded · Dec 16, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > APU COMPARTMENT RT TORQUE BOX SUPPORT ANGLE LOCATED AFT OF AFT AIR INLET CUTOUT HAS MID ATTACH CLIP CORROSION AND TWO ATTACH FASTENERS MISSING. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR ASAA2013121212232](https://openairdocs.org/sdr/ASAA2013121212232.md): Stringer · corroded · Dec 12, 2013 · N778AS · Boeing 7374Q8 · Fuselage Main, Longeron/Stringer
  > APU RT TORQUE BOX AREA, APU INLET CUTOUT LWR STRINGER IS CORRODED, ACFT GROUNDED. BLENDED DAMAGED AREA REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED STRINGER AND INSTALLED NEW STRINGER IAW SRM 51-40-02-0G-0.
- [SDR ASAA2013121112260](https://openairdocs.org/sdr/ASAA2013121112260.md): Beam · cracked · Dec 11, 2013 · N778AS · Boeing 7374Q8 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER CENTER SECTION LT THRUST BEAM LOWER OTBD CORNER FITTING IS CRACKED ON HORIZONTAL FLANGE. COMPLIED WITH T/C SB737-55-1091-400-1 FOR LEFT SIDE THRUST BEAM CORNER FITTING REPLACEMENT ONLY IAW EA 400-55EA-11823.
- [SDR ASAA2013121012221](https://openairdocs.org/sdr/ASAA2013121012221.md): Support Angle · corroded · Dec 10, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY LT TRANSITION ANGLE HAS CORROSION FROM BS 767 TO 817. REMOVED CORROSION IAW SRM 53-60-53-1A-1. REPAIRED ANGLE IAW SRM 53-60-53-2R-4, REP 4.
- [SDR ASAA2013120612306](https://openairdocs.org/sdr/ASAA2013120612306.md): Structure · corroded · Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > APU BAY RT SIDE AFT AIR INLET DUCT CUTOUT SURROUND LANDING HAS MULTIPLE CORROSION AREAS. ACFT GROUNDED. REMOVED AND INSTALLED NEW TEE IAW SRM 51-40-02.
- [SDR ASAA2013120612291](https://openairdocs.org/sdr/ASAA2013120612291.md): Support Angle · corroded · Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > APU COMPARTMENT, RT AFT AIR INLET CUTOUT, AFT SUPPORT ANGLE CORRODED. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR ASAA2013120612290](https://openairdocs.org/sdr/ASAA2013120612290.md): Support Angle · corroded · Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > APU COMPARTMENT ON RT WEB ANGLE BETWEEN TWO CUTOUTS HAS CORROSION ON AFT END. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR ASAA2013120612284](https://openairdocs.org/sdr/ASAA2013120612284.md): Attach Angle · corroded · Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Main, Attach Fittings
  > APU COMPARTMENT RT TORQUE BOX WEB SUPPORT FRAME BS 1129, MID ATTACH ANGLE HAS CORROSION. ACFT GROUNDED. REMOVED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02.
- [SDR ASAA2013120612176](https://openairdocs.org/sdr/ASAA2013120612176.md): Tee Fitting · corroded · Dec 6, 2013 · N778AS · Boeing 7374Q8 · APU Cowling/Containment
  > ON BACK SIDE OF APU COMPARTMENT, RT WEB, THE SUPPORT FRAME FWD OF THE AFT CUTOUT HAS MID ATTACHMENT ANGLE CORRODED. ACFT GROUNDED. R & R TEE ANGLE IAW SRM 51-40-02, W.5", O.094, R.049", L.5", D.045".
- [SDR ASAA2013120412302](https://openairdocs.org/sdr/ASAA2013120412302.md): Pan · corroded · Dec 4, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > POTABLE WATER SERVICE CUT OUT BOX CORRODED AROUND THE WATER FILL LINE ATTACHMENT STA 947.5 TO 967, STGR26L TO STGR25L. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1, FIG 101. R & R POTABLE WATER CUTOUT BOX PAN IAW SRM 51-4
- [SDR ASAA2013120412242](https://openairdocs.org/sdr/ASAA2013120412242.md): Shear Tie · corroded · Dec 4, 2013 · N778AS · Boeing 7374Q8 · Fuselage Internal Mounting Structure
  > FRAME BS 967 SHEAR TIE CORRODED BETWEEN S25-26L REMOVED CORROSION AND FOUND SHEAR TIE OUT OF LIMITS IAW SRM 53-00-07-1A-1 ALLOWABLE DAMAGE. R & R SHEAR TIE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2013120412233](https://openairdocs.org/sdr/ASAA2013120412233.md): Shear Tie · corroded · Dec 4, 2013 · N778AS · Boeing 7374Q8 · Fuselage Internal Mounting Structure
  > FRAME BS 967 SHEAR TIE CORRODED BETWEEN S25-26L. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND SHEAR TIE OUT OF LIMITS IAW SRM 53-00-07-1A-1. ALLOWABLE DAMAGE R & R SHEAR TIE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2013120212258](https://openairdocs.org/sdr/ASAA2013120212258.md): Structure · chafed · Dec 2, 2013 · N778AS · Boeing 7374Q8 · Trailing Edge Flaps
  > RIGHT OTBD MID FLAP L/E IS CHAFED BY NR 7 FLAP TRACK. REPAIRED RT OTBD MIDFLAP L/E BY NR 7 FLAP TRACK FAIRING IAW EA 15482, REV IR, DATE 20DEC13 AND EA 400-57EA-11877.
- [SDR ASAA2013120212175](https://openairdocs.org/sdr/ASAA2013120212175.md): Skin · damaged · Dec 2, 2013 · N778AS · Boeing 7374Q8 · Leading Edge Devices
  > LT NR 2 SLAT OTBD BOTTOM EDGE IS DAMAGED. ACFT GROUNDED. REPAIRED LT NR 2 SLAT OTBD BOTTOM EDGE IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2013120112257](https://openairdocs.org/sdr/ASAA2013120112257.md): Skin · chafed · Dec 1, 2013 · N778AS · Boeing 7374Q8 · Trailing Edge Flaps
  > RIGHT WING OTBD FOREFLAP INBD L/E IS CHAFED. R & R RT WING OTBD FOREFLAP INBD L/E SKIN IAW SRM 51-40-02-0G-0.
- [SDR ASAA2013090795932](https://openairdocs.org/sdr/ASAA2013090795932.md): Cover · dislodged · Sep 7, 2013 · N778AS · Boeing 7374Q8 · Emergency Lighting
  > EXIT SIGN COVER ON CEILING JUST AFT OF COCKPIT DOOR FELL OFF. ACFT GROUNDED. RESECURED SIGN COVER, OK FOR SERVICE.
- [SDR ASAA2013081895838](https://openairdocs.org/sdr/ASAA2013081895838.md): Guide Arm · failed · Aug 18, 2013 · N778AS · Boeing 7374Q8 · Passenger/Crew Doors
  > L1 LWR HINGE COVER BINDING DURING DOOR CLOSURE. ACFT GROUNDED. FOUND UPPER AFT DOOR DAMAGE. UPPER AFT DOOR DAMAGE REMOVED. REPLACED GUIDE ARM, ADJUSTED DOOR. OPS CHK GOOD IAW MM 52-11-21 INSTALLED GUIDE ARM IAW 52-11-21-404-007.
- [SDR ASAA2013081595803](https://openairdocs.org/sdr/ASAA2013081595803.md): Guide Arm · out of adjust · Aug 15, 2013 · N778AS · Boeing 7374Q8 · Passenger/Crew Doors
  > F/A REPORTED THAT THE L1 DOOR IS HARD TO CLOSE. ACFT GROUNDED. FOUND UPPER GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED UPPER GUIDE ARM IAW MM 52-11-00-705-007, STEP 3.G. FORCE CHECKED OK IAW MM 52-11-00-755-051.
- [SDR ASAA2013040794405](https://openairdocs.org/sdr/ASAA2013040794405.md): Web · corroded · Apr 7, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > LT WHEEL WELL CUT OUT VERTICAL WEB CORRODED AFT SIDE 6 O`CLOCK TO 9 O`CLOCK POSITION. REPAIRED VERTICAL WEB IAW EA 400 53EA 10105 REV NEW ISSUED DATE 09APR13.
- [SDR ASAA2013040694382](https://openairdocs.org/sdr/ASAA2013040694382.md): Web · corroded · Apr 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
  > LT MAIN W/W AFT LOWER CHORD HAS FRETTING AND CORROSION. ACFT GROUNDED. REMOVED FASTENERS AND N/PS FROM LT W/W AFT LOWER CHORD, REINSTALLED FASTENERS AND N/PS ONTO LT W/W AFT LOWER CHORD. REPAIRED VERTICAL WEB IAW EA 53EA 10105 REV NEW.
- [SDR ASAA2012090992919](https://openairdocs.org/sdr/ASAA2012090992919.md): Channel · corroded · Sep 9, 2012 · N778AS · Boeing 7374Q8 · Horizontal Stabilizer Miscellaneous Structure
  > AFT TAIL COMPARTMENT JACKSCREW SUPPORT FITTINGS LOWER BOX BRACE CHANNEL IS CORRODED. ACFT GROUNDED. REMOVED CORRODED CHANNEL IAW SRM 51-40-02. FABRICATED NEW SUPPORT CHANNEL IAW BAC DWG 69-56190, REV A. ALODINED AND PRIMED NEW SUPPORT CHANNEL IAW BAC DWG
- [SDR ASAA12411551](https://openairdocs.org/sdr/ASAA12411551.md): Light · broken · May 11, 2012 · N778AS · Boeing 7374Q8 · Emergency Lighting
  > R1 DOOR LOWER EMERGENCY EXIT LIGHT ASSY IS BROKEN. REMOVED & INSTALLED R1 DOOR LOWER EMERGENY EXIT LIGHT ASSY OPS NORMAL, REF 33-51-02.

Next page: https://openairdocs.org/deregistered/N778AS-2017-02-13/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 = 'N778AS' AND deregistration_id = 'N778AS-2017-02-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N778AS-2017-02-13/reports

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