# Service difficulty reports: N977AS, cancelled Jun 17, 2014

A list on [N977AS, cancelled Jun 17, 2014](https://openairdocs.org/deregistered/N977AS-2014-06-17.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 3 · 103 reports

- [SDR ASAA0782259](https://openairdocs.org/sdr/ASAA0782259.md): Vane · dented · Nov 18, 2007 · N977AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT I/B FLAP I/B VANE DENTED AT TOP SURFACE IN MIDDLE SECTION OF VANE. REMOVED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER PREPARED AREA BAND AREA AND FASTENERS IAW MD80 SRM 51-70-2 PGS 11, 23, 43, 45, 59 AND 63.
- [SDR ASAA0782258](https://openairdocs.org/sdr/ASAA0782258.md): Skin · dented · Nov 18, 2007 · N977AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT FLAP I/B SIDE I/B FLAP VANE MULTIPLE DENTS ON LWR. REMOVED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER, PREPARED AREA BOND AREA AND FASTENER IAW MD80 SRM 51-70-2 PG 11, 23, 43, 45, 59 AND 63.
- [SDR ASAA0782257](https://openairdocs.org/sdr/ASAA0782257.md): Skin · dented · Nov 18, 2007 · N977AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT WING I/B FLAP O/B VANE MULTIPLE DENTS ON LWR I/B SURFACE. PREPARED DAMAGED AREA IAW MD 80 SRM 51-70-2 PG 11. FABRICATED DOUBLER AND BONDED IAW MD 80 SRM 51-70-2 PGS 23 AND 91.
- [SDR ASAA0782260](https://openairdocs.org/sdr/ASAA0782260.md): Frame · cracked · Nov 18, 2007 · N977AS · Doug DC983 · Fuselage Main, Frame
  > AFT ACCESSORY COMPT FRAME STA 1418 CRACKED IN RADIUS AT LONG 2R AND LONG 2L. TWO EACH CRACKS PREPARED DAMAGED AREA, STOP DRILLED CRACKS, VERIFIED CRACK TERMINATION IAW MD80 SRM 51-01 PG 9. RECEIVED REPLACEMENT REPAIR PARTS LOCATED, DRILLED AND INSTALLED IAW
- [SDR ASAA0782253](https://openairdocs.org/sdr/ASAA0782253.md): Skin · gouged · Nov 15, 2007 · N977AS · Doug DC983 · Trailing Edge Flaps
  > RIGHT WING O/B FLAP I/B VANE PREVIOUS REPAIR GOUGED. REMOVED DAMAGED DOUBLER. FABRICATED, LOCATED, DRILLED AND BONDED REPAIR DOUBLER AND FILLER IAW MD80 SRM 51-70-2 PAR 18B AND 57-03 FIG 11 PG 27.
- [SDR ASAA0782252](https://openairdocs.org/sdr/ASAA0782252.md): Skin · damaged · Nov 15, 2007 · N977AS · Doug DC983 · Trailing Edge Flaps
  > LEFT WING O/B FLAP I/B VANE REPAIR DOUBLER GOUGED. REMOVED DAMAGED REPAIR DOUBLER, FABRICATED, LOCATED, DRILLED AND BONDED IAW MD80 SRM 51-70-2 PAR 18B PG 91 AND MD80 SRM 57-03 FIG 11 PG 27.
- [SDR ASAA0782251](https://openairdocs.org/sdr/ASAA0782251.md): Longeron · cracked · Nov 14, 2007 · N977AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPT LONGERON 2L CRACKED AT AFT SIDE OF FRAME 1418. REMOVED DAMAGED SECTION OF LONGERON LOCATED DRILLED AND INSTALLED REPAIR EXTRUSION AND REPAIR SPLICE IAW MD80 SRM 53-02 FIG 18.
- [SDR ASAA0782250](https://openairdocs.org/sdr/ASAA0782250.md): Longeron · cracked · Nov 14, 2007 · N977AS · Doug DC983 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPT LONGERON 2R CRACKED AT AFT SIDE OF FRAME STA 1418. REMOVED DAMAGED SECTION OF LONGERON, LOCATED, DRILLED AND INSTALLED REPAIR EXTRUSION AND REPAIR SPLICE IAW MD80 SRM 53-02 FIG 18.
- [SDR ASAA0782228](https://openairdocs.org/sdr/ASAA0782228.md): Shear Tie · cracked · Nov 12, 2007 · N977AS · Doug DC983 · Fuselage Internal Mounting Structure
  > AFT ACCESSORY COMPT SHEAR TIE CRACKED AT AFT SIDE OF FRAME STA 1437 I/B OF LONGERON 3R. REMOVED DAMAGED SHEAR TIE RECEIVED A REPLACEMENT SHEAR TIE, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 PG 1 AND FIG 3A SHEET 1 AND 51-30-5 PG 12, 13.
- [SDR ASAA0782227](https://openairdocs.org/sdr/ASAA0782227.md): Shear Tie · cracked · Nov 12, 2007 · N977AS · Doug DC983 · Fuselage Internal Mounting Structure
  > AFT ACCESSORY COMPT SHEAR TIE CRACKED AT AFT SIDE OF FRAME STA 1437 I/B OF LONGERON 3L. REMOVED DAMAGED SHEAR TIE RECEIVED A REPLACEMENT SHEAR TIE LOCATED DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 PG 1 AND FIG 3A SHEET 1 AND 51-30-5 PG 12 AND 13.
- [SDR ASAA0782226](https://openairdocs.org/sdr/ASAA0782226.md): Floor Panel · delaminated · Nov 9, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED AT STA 866 TO STA 887 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
- [SDR ASAA0782225](https://openairdocs.org/sdr/ASAA0782225.md): Floor Panel · delaminated · Nov 9, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL PUNCTURED DENTED APPROX IN MIDDLE OF PANEL STA 826 TO STA 927 LBL 44 TO LBL 54. REMOVED DAMAGED AREA, FABRICATED LOCATED DRILLED AND INSTALLED A REPAIR DOUBLER IAW MD80 SRM 53 01 FIG 4 SHEET 4.
- [SDR ASAA0782229](https://openairdocs.org/sdr/ASAA0782229.md): Skin · dented · Nov 8, 2007 · N977AS · Doug DC983 · Ailerons
  > LEFT AILERON IS DENTED APPROX 2 INCHES FORWARD OF TRIM TAB O/B HINGE LOWER SURFACE. PREPARED DAMAGED AREA IAW MD80 SRM 51-90-0 PG 9, APPLIED LAYER OF MIL C 9084 FIBERGLASS BONDED REPAIR IAW MD80 SRM 51-90-0 PG 44.
- [SDR ASAA0782224](https://openairdocs.org/sdr/ASAA0782224.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL HAT STIFFENER CREASED ON AFT SIDE AND PANEL HAS 1 INCH CRACK IN CENTER AREA STA 826 TO STA 928 RBL 44 TO RBL 54. REMOVED DAMAGED HAT CHANNEL, INSTALLED A REPLACEMENT CHANNEL IAW MD80 SRM 51-10-4 PG 1 & 51-30-2 PG 1. REPAIRED CRACK IAW MD80
- [SDR ASAA0782223](https://openairdocs.org/sdr/ASAA0782223.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED STA 826 TO STA 866 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
- [SDR ASAA0782221](https://openairdocs.org/sdr/ASAA0782221.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED STA 887 TO STA 927 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
- [SDR ASAA0782220](https://openairdocs.org/sdr/ASAA0782220.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED STA 927 TO STA 1003 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD 80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
- [SDR ASAA0782219](https://openairdocs.org/sdr/ASAA0782219.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED STA 887 TO STA 927 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
- [SDR ASAA0782218](https://openairdocs.org/sdr/ASAA0782218.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED STA 826 TO STA 866 RBL 22 TP RBL 44. FABRICATED A REPLACEMENT PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
- [SDR ASAA0782217](https://openairdocs.org/sdr/ASAA0782217.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOORBOARD CRACKED OUT CORNER AND DELAMINATED STA 927 TO STA 1003 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWINGS S4932106.
- [SDR ASAA0782216](https://openairdocs.org/sdr/ASAA0782216.md): Floor Panel · delaminated · Nov 8, 2007 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED STA 769 TO STA 807 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWINGS S4932106.
- [SDR ASAA0782193](https://openairdocs.org/sdr/ASAA0782193.md): Skin · dented · Nov 4, 2007 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > RIGHT EXTERNAL FUSELAGE SKIN DENTED 27 INCHES BELOW PYLON STA 1308 DENT MEASURES.700 DIA DEPTH.032 RATIO OF 21.8 COLD WORKED DENT IAW MD80 SRM 53-04 FIG 38. EDDY CURRENT INSPECTED COLD WORKED AREA NO CRACKS NOTED IAW MD80 NTSPM 06 10 00.001 PROCEDURE 1. FA
- [SDR ASAA0781444](https://openairdocs.org/sdr/ASAA0781444.md): Csd · overtemp · Feb 5, 2007 · N977AS · Doug DC983 · Alternator-Generator Drive
  > LEFTHAND ENGINE CSD TEMPERATURE IN RED DURING CLIMB FROM ANC. SHUTDOWN CSD AND DIVERTED TO FAI. REPLACED CSD.
- [SDR ASAA0681140](https://openairdocs.org/sdr/ASAA0681140.md): Slide · failed · Oct 24, 2006 · N977AS · Doug DC983 · Escape Slide
  > DURING CATERING, THE L 2 DOOR SLIDE PACK FELL OUT OF SLIDE CASE AND WOULD NOT DEPLOY. FOR MORE INFO NEED TO NOTIFY INFLT SERVICE FOR DETAILS. CLARIFICATION OF CIRCUMSTANCES SURROUNDING THIS INCIDENT HAS BEEN REQUESTED FROM LINE MAINTENANCE AND IT IS INTENDED
- [SDR ASAA0680861](https://openairdocs.org/sdr/ASAA0680861.md): Skin · gouged · Aug 10, 2006 · N977AS · Doug DC983 · Trailing Edge Flaps
  > FOUND RIGHT WING OUTBOARD FLAP INBOARD VANE IS GOUGED. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER PER SRM 51 70 2.
- [SDR ASAA0680860](https://openairdocs.org/sdr/ASAA0680860.md): Skin · gouged · Aug 10, 2006 · N977AS · Doug DC983 · Trailing Edge Flaps
  > FOUND LEFT WING OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT DOUBLER AND FILLER PER SRM 51 70 2.
- [SDR ASAA0680859](https://openairdocs.org/sdr/ASAA0680859.md): Skin · dented · Aug 10, 2006 · N977AS · Doug DC983 · Trailing Edge Flaps
  > FOUND LEFT WING OUTBOARD FLAP OUTBOARD VANE DENTED. REMOVED DAMAGED VANE SKIN. INSTALLED SKIN FILLER AND EXTERNAL REPAIR DOUBLER PER SRM 57 03 AND 51 70 2.
- [SDR ASAA0680858](https://openairdocs.org/sdr/ASAA0680858.md): Skin · dented · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENTED. COLD FORMED TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
- [SDR ASAA0680857](https://openairdocs.org/sdr/ASAA0680857.md): Skin · dented · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION PER SRM 53 04.
- [SDR ASAA0680856](https://openairdocs.org/sdr/ASAA0680856.md): Skin · dented · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENTED. COLD FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
- [SDR ASAA0680855](https://openairdocs.org/sdr/ASAA0680855.md): Skin · corroded · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER INTERNAL FINGER DOUBLER AND AN EXTERNAL REPAIR DOUBLER PER ASA EA 5330 02129.
- [SDR ASAA0680854](https://openairdocs.org/sdr/ASAA0680854.md): Skin · gouged · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER PER SRM 53 04.
- [SDR ASAA0680853](https://openairdocs.org/sdr/ASAA0680853.md): Skin · dented · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENTED. COLD FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
- [SDR ASAA0680852](https://openairdocs.org/sdr/ASAA0680852.md): Floor Panel · delaminated · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680851](https://openairdocs.org/sdr/ASAA0680851.md): Floor Panel · damaged · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL CORE DAMAGED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680850](https://openairdocs.org/sdr/ASAA0680850.md): Floor Panel · damaged · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > FOUND CABIN FLOOR PANEL CORE DAMAGED AT INSERT HOLES. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680849](https://openairdocs.org/sdr/ASAA0680849.md): Floor Panel · delaminated · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680848](https://openairdocs.org/sdr/ASAA0680848.md): Floor Panel · delaminated · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680847](https://openairdocs.org/sdr/ASAA0680847.md): Floor Panel · delaminated · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DELAMINATED AND HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680846](https://openairdocs.org/sdr/ASAA0680846.md): Floor Panel · damaged · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > FOUND CABIN FLOOR PANEL CORE DAMAGED AT INSERTS. REPLACED PANEL PER SRM 53 05.
- [SDR ASAA0680845](https://openairdocs.org/sdr/ASAA0680845.md): Floor Panel · damaged · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Floor Panel
  > CABIN FLOOR PANEL DAMAGED AT INSERT HOLES. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680844](https://openairdocs.org/sdr/ASAA0680844.md): Beam · corroded · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Main, Structure
  > AFT CARGO BAY DOOR CUTOUT LOWER BEAM CORRODED. REPLACED BEAM PER SRM 51 10 4 51 30 2 AND 51 30 5.
- [SDR ASAA0680843](https://openairdocs.org/sdr/ASAA0680843.md): Intercostal · corroded · Aug 10, 2006 · N977AS · Doug DC983 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 51 30 2 AND 51 30 5.
- [SDR ASAA0680842](https://openairdocs.org/sdr/ASAA0680842.md): Intercostal · cracked · Aug 10, 2006 · N977AS · Doug DC983 · Passenger/Crew Doors
  > FOUND FORWARD ENTRY DOOR HAS CRACKED INTERCOSTAL BEHIND HANDLE MECHANISM. REPLACED INTERCOSTAL PER SRM 51 10 4 51 30 2 AND 51 30 5.
- [SDR ASAA0580471](https://openairdocs.org/sdr/ASAA0580471.md): Vane · chafed · Aug 17, 2005 · N977AS · Doug DC983 · Trailing Edge Flaps
  > OKC - FOUND LEFT WING OUTBOARD FLAP INBOARD VANE EXTERNAL DOUBLER IS CHAFED. REMOVED DOUBLER. INSTALLED REPLACEMENT DOUBLER. INSTALLED REPLACEMENT DOUBLER. (M)
- [SDR ASAA0580470](https://openairdocs.org/sdr/ASAA0580470.md): Skin · dented · Aug 17, 2005 · N977AS · Doug DC983 · Fuselage Main, Plate/Skin
  > OKC - FOUND DURING C-CHECK, FUSELAGE DENTED. REMOVED DAMAGED AREA. INSTALLED INTERNAL AND EXTERNAL DOUBLERS. (M)
- [SDR ASAA0580469](https://openairdocs.org/sdr/ASAA0580469.md): Support · cracked · Aug 17, 2005 · N977AS · Doug DC983 · Fuselage Miscellaneous Structure
  > OKC - DURING C-CHECK, FOUND NOSE LANDING GEAR WHEELWELL LEFT SUPPORT FRAME UPPER FASTENER CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR ANGLE, SHIM, AND CLIP
- [SDR ASAA0580468](https://openairdocs.org/sdr/ASAA0580468.md): Support · cracked · Aug 17, 2005 · N977AS · Doug DC983 · Fuselage Miscellaneous Structure
  > OKC - DURING C-CHECK, FOUND NOSE LANDING GEAR WHEELWELL RIGHT SUPPORT FRAME UPPER FASTENER CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR ANGLE, SHIM, AND CLIP. (M)
- [SDR ASAA0580467](https://openairdocs.org/sdr/ASAA0580467.md): Skin · dented · Aug 17, 2005 · N977AS · Doug DC983 · Cargo/Baggage Doors
  > OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED ONE EXTERNAL DOUBLER, TWO INTERNAL DOUBLERS, AND THREE FILLERS. (M)
- [SDR ASA0580466](https://openairdocs.org/sdr/ASA0580466.md): Skin · dented · Aug 17, 2005 · N977AS · Doug DC983 · Cargo/Baggage Doors
  > OKC - DURING C-CHECK, FOUND MID CARGO BAY DOOR SKIN IS DENTED. COLD-FORMED SKIN. INSTALLED REPAIR DOUBLER. (M)

Next page: https://openairdocs.org/deregistered/N977AS-2014-06-17/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 = 'N977AS' AND deregistration_id = 'N977AS-2014-06-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N977AS-2014-06-17/reports

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