# N977AS: 1995 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2014-06-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 17, 2014
- Exported to: Venezuela
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 53453
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 24, 1995
- Certificate issued: May 23, 2013
- Last registry action: May 23, 2013
- Mode S code: AD9DB7
- Owner when cancelled: [Air Capital Group LLC](https://openairdocs.org/faa-owner/AIR%20CAPITAL%20GROUP%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N977AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=977AS
- Page: https://openairdocs.org/deregistered/N977AS-2014-06-17

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md

## Service difficulty reports (103, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASAA0782259](https://openairdocs.org/sdr/ASAA0782259), Nov 18, 2007: VANE. DENTED. 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 
- [SDR ASAA0782258](https://openairdocs.org/sdr/ASAA0782258), Nov 18, 2007: SKIN. DENTED. 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 MD
- [SDR ASAA0782257](https://openairdocs.org/sdr/ASAA0782257), Nov 18, 2007: SKIN. DENTED. 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 5
- [SDR ASAA0782260](https://openairdocs.org/sdr/ASAA0782260), Nov 18, 2007: FRAME. CRACKED. 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 TERMINAT
- [SDR ASAA0782253](https://openairdocs.org/sdr/ASAA0782253), Nov 15, 2007: SKIN. GOUGED. 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-
- [SDR ASAA0782252](https://openairdocs.org/sdr/ASAA0782252), Nov 15, 2007: SKIN. DAMAGED. 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 AN
- [SDR ASAA0782251](https://openairdocs.org/sdr/ASAA0782251), Nov 14, 2007: LONGERON. CRACKED. 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
- [SDR ASAA0782250](https://openairdocs.org/sdr/ASAA0782250), Nov 14, 2007: LONGERON. CRACKED. 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 
- [SDR ASAA0782228](https://openairdocs.org/sdr/ASAA0782228), Nov 12, 2007: SHEAR TIE. CRACKED. 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, DRI
- [SDR ASAA0782227](https://openairdocs.org/sdr/ASAA0782227), Nov 12, 2007: SHEAR TIE. CRACKED. 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 DRILL
- [SDR ASAA0782226](https://openairdocs.org/sdr/ASAA0782226), Nov 9, 2007: FLOOR PANEL. DELAMINATED. 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
- [SDR ASAA0782225](https://openairdocs.org/sdr/ASAA0782225), Nov 9, 2007: FLOOR PANEL. DELAMINATED. 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
- [SDR ASAA0782229](https://openairdocs.org/sdr/ASAA0782229), Nov 8, 2007: SKIN. DENTED. 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
- [SDR ASAA0782224](https://openairdocs.org/sdr/ASAA0782224), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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, 
- [SDR ASAA0782223](https://openairdocs.org/sdr/ASAA0782223), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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 S4
- [SDR ASAA0782221](https://openairdocs.org/sdr/ASAA0782221), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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 S4
- [SDR ASAA0782220](https://openairdocs.org/sdr/ASAA0782220), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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 
- [SDR ASAA0782219](https://openairdocs.org/sdr/ASAA0782219), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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 S4
- [SDR ASAA0782218](https://openairdocs.org/sdr/ASAA0782218), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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 A
- [SDR ASAA0782216](https://openairdocs.org/sdr/ASAA0782216), Nov 8, 2007: FLOOR PANEL. DELAMINATED. 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 S
- [SDR ASAA0782193](https://openairdocs.org/sdr/ASAA0782193), Nov 4, 2007: SKIN. DENTED. 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. E
- [SDR ASAA0781444](https://openairdocs.org/sdr/ASAA0781444), Feb 5, 2007: CSD. OVERTEMP. 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), Oct 24, 2006: SLIDE. FAILED. 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 C
- [SDR ASAA0680861](https://openairdocs.org/sdr/ASAA0680861), Aug 10, 2006: SKIN. GOUGED. FOUND RIGHT WING OUTBOARD FLAP INBOARD VANE IS GOUGED. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER PER S
- [SDR ASAA0680860](https://openairdocs.org/sdr/ASAA0680860), Aug 10, 2006: SKIN. GOUGED. FOUND LEFT WING OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT DOUBLER AND F
- [SDR ASAA0680859](https://openairdocs.org/sdr/ASAA0680859), Aug 10, 2006: SKIN. DENTED. 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), Aug 10, 2006: SKIN. DENTED. FOUND FUSELAGE SKIN DENTED. COLD FORMED TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
- [SDR ASAA0680857](https://openairdocs.org/sdr/ASAA0680857), Aug 10, 2006: SKIN. DENTED. FOUND FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION PER SRM 53 04.
- [SDR ASAA0680856](https://openairdocs.org/sdr/ASAA0680856), Aug 10, 2006: SKIN. DENTED. 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), Aug 10, 2006: SKIN. CORRODED. 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), Aug 10, 2006: SKIN. GOUGED. 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), Aug 10, 2006: SKIN. DENTED. 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), Aug 10, 2006: FLOOR PANEL. DELAMINATED. FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680851](https://openairdocs.org/sdr/ASAA0680851), Aug 10, 2006: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL CORE DAMAGED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680850](https://openairdocs.org/sdr/ASAA0680850), Aug 10, 2006: FLOOR PANEL. DAMAGED. 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), Aug 10, 2006: FLOOR PANEL. DELAMINATED. FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680848](https://openairdocs.org/sdr/ASAA0680848), Aug 10, 2006: FLOOR PANEL. DELAMINATED. CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680847](https://openairdocs.org/sdr/ASAA0680847), Aug 10, 2006: FLOOR PANEL. DELAMINATED. 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), Aug 10, 2006: FLOOR PANEL. DAMAGED. FOUND CABIN FLOOR PANEL CORE DAMAGED AT INSERTS. REPLACED PANEL PER SRM 53 05.
- [SDR ASAA0680845](https://openairdocs.org/sdr/ASAA0680845), Aug 10, 2006: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL DAMAGED AT INSERT HOLES. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
- [SDR ASAA0680844](https://openairdocs.org/sdr/ASAA0680844), Aug 10, 2006: BEAM. CORRODED. 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), Aug 10, 2006: INTERCOSTAL. CORRODED. 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), Aug 10, 2006: INTERCOSTAL. CRACKED. 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), Aug 17, 2005: VANE. CHAFED. 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), Aug 17, 2005: SKIN. DENTED. OKC - FOUND DURING C-CHECK, FUSELAGE DENTED. REMOVED DAMAGED AREA. INSTALLED INTERNAL AND EXTERNAL DOUBLERS. (M)
- [SDR ASAA0580469](https://openairdocs.org/sdr/ASAA0580469), Aug 17, 2005: SUPPORT. CRACKED. 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), Aug 17, 2005: SUPPORT. CRACKED. OKC - DURING C-CHECK, FOUND NOSE LANDING GEAR WHEELWELL RIGHT SUPPORT FRAME UPPER FASTENER CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR ANGLE, SHIM, AND CLIP. 
- [SDR ASAA0580467](https://openairdocs.org/sdr/ASAA0580467), Aug 17, 2005: SKIN. DENTED. 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. (
- [SDR ASA0580466](https://openairdocs.org/sdr/ASA0580466), Aug 17, 2005: SKIN. DENTED. OKC - DURING C-CHECK, FOUND MID CARGO BAY DOOR SKIN IS DENTED. COLD-FORMED SKIN. INSTALLED REPAIR DOUBLER. (M)

All 103: https://openairdocs.org/deregistered/N977AS-2014-06-17/reports.md

---
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.