# N997DL: 1992 Mcdonnell Douglas MD-88

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-88](https://openairdocs.org/model/mcdonnell-douglas-md-88) (registry code 3023688, 142 seats)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 53364
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 22, 1992
- Certificate issued: February 24, 2023
- Expires: February 28, 2030
- Mode S code: ADECFA
- Registered owner: [Tatonduk Outfitters Ltd](https://openairdocs.org/faa-owner/TATONDUK%20OUTFITTERS%20LTD)
- Location: [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks)
- Owner type: Corporation
- Owner's area on the map: 64.8774° N, 148.1486° W: Placed by OpenAirDocs at the center of ZIP code 99709, within about 13 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=997DL
- Page: https://openairdocs.org/aircraft/N997DL

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Pratt & Whitney JT8D model are included.

## ADs that may apply (OpenAirDocs): 217 in force

### Matched by airframe (Mcdonnell Douglas MD-88)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-09-11](https://openairdocs.org/ad/2025-09-11): Flight controls · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 20 more. Effective Jun 12, 2025
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-02-09](https://openairdocs.org/ad/2023-02-09): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Mar 20, 2023
- [AD 2023-01-13](https://openairdocs.org/ad/2023-01-13): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Mar 13, 2023
- [AD 2020-10-10](https://openairdocs.org/ad/2020-10-10): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jun 26, 2020
- [AD 2018-07-04](https://openairdocs.org/ad/2018-07-04): Ice and rain protection · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective Sep 10, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-17-19](https://openairdocs.org/ad/2017-17-19): Fuselage · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Oct 4, 2017
- [AD 2016-25-06](https://openairdocs.org/ad/2016-25-06): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jan 25, 2017
- [AD 2016-03-06](https://openairdocs.org/ad/2016-03-06): Fuel · Boeing DC-9-11, DC-9-12, DC-9-13 and 21 more. Effective Mar 23, 2016
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-21-04](https://openairdocs.org/ad/2014-21-04): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Dec 2, 2014
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2013-05-02](https://openairdocs.org/ad/2013-05-02): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Apr 15, 2013
- [AD 2012-21-13](https://openairdocs.org/ad/2012-21-13): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Dec 4, 2012
- [AD 2011-17-11](https://openairdocs.org/ad/2011-17-11): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 26, 2011
- [AD 2011-15-01](https://openairdocs.org/ad/2011-15-01): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Aug 19, 2011
- [AD 2011-14-03](https://openairdocs.org/ad/2011-14-03): Stabilizers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Aug 10, 2011
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-16](https://openairdocs.org/ad/2011-01-16): Fuel · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Feb 16, 2011
- [AD 2010-25-04](https://openairdocs.org/ad/2010-25-04): Compliance · Boeing DC-9-31, DC-9-32, DC-9-32 (VC-9C) and 14 more. Effective Jan 11, 2011
- [AD 2009-15-16 R1](https://openairdocs.org/ad/2009-15-16-R1): Doors · Intrusion/Penetration Resistance Flightdeck Door and Reinforced… (Aircraft Reconfig Technologies STC ST02463AT). Effective Aug 5, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-13-29](https://openairdocs.org/ad/2008-13-29): Overwing frames · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Aug 12, 2008
- [AD 2008-06-27](https://openairdocs.org/ad/2008-06-27): Evacuation system's shear-pin · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 91 more. Effective Apr 28, 2008
- [AD 2008-03-12](https://openairdocs.org/ad/2008-03-12): Rudder pedal bracket · Boeing DC-8-11, DC-8-12, DC-8-21 and 47 more. Effective Mar 11, 2008
- [AD 2007-17-18](https://openairdocs.org/ad/2007-17-18): Static port heater assemblies · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Oct 2, 2007
- [AD 2006-16-02](https://openairdocs.org/ad/2006-16-02): Refueling Manifold · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 7, 2006
- [AD 2006-15-15](https://openairdocs.org/ad/2006-15-15): Wire bundle for the auxiliary hydraulic pump · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 5, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2006-07-11](https://openairdocs.org/ad/2006-07-11): Aft attach fitting assembly of the spoiler link · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective May 5, 2006
- [AD 2006-01-02](https://openairdocs.org/ad/2006-01-02): Upper lock link assembly of the nose landing gear (NLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Feb 22, 2006
- [AD 2005-13-18](https://openairdocs.org/ad/2005-13-18): Battery terminal screws · Boeing DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Aug 1, 2005
- [AD 2005-09-04](https://openairdocs.org/ad/2005-09-04): Main landing gear (MLG) shock strut pistons · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jun 2, 2005
- [AD 2004-25-14](https://openairdocs.org/ad/2004-25-14): Main landing gear (MLG) · Boeing DC-9-14, DC-9-15, DC-9-15F and 17 more. Effective Jan 20, 2005
- [AD 2004-23-21](https://openairdocs.org/ad/2004-23-21): Power feeder cables of the auxiliary power unit (APU) · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jan 3, 2005
- [AD 2004-23-05](https://openairdocs.org/ad/2004-23-05): Ground stud installation of the main battery · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Dec 20, 2004
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-15-13](https://openairdocs.org/ad/2004-15-13): Freeze Protection Ribbon Heaters · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Sep 2, 2004
- [AD 2004-13-23](https://openairdocs.org/ad/2004-13-23): Seat track locking pins · Boeing DC-9-82 (MD-82), DC-9-83 (MD-83) and MD-88. Effective Aug 13, 2004
- [AD 2004-11-07](https://openairdocs.org/ad/2004-11-07): Structural Integrity · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jul 9, 2004
- [AD 2004-05-25](https://openairdocs.org/ad/2004-05-25): Seat Locking Pins · Boeing DC-9-14, DC-9-15, DC-9-15F and 18 more. Effective Apr 19, 2004
- [AD 2004-05-09](https://openairdocs.org/ad/2004-05-09): Forward cargo compartment · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Apr 7, 2004
- [AD 2004-05-03](https://openairdocs.org/ad/2004-05-03): Shock strut cylinders · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 3 more. Effective Mar 15, 2004
- [AD 2004-02-09](https://openairdocs.org/ad/2004-02-09): Discrepant circuit breakers · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Mar 5, 2004
- [AD 2003-24-14](https://openairdocs.org/ad/2003-24-14): Electrical Wiring Installations in Various Areas of the Airplane · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Jan 8, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003

### Matched by engine (Pratt & Whitney JT8D series)

- [AD 2021-22-19](https://openairdocs.org/ad/2021-22-19): Turbine Engine Compressor Section · Pratt & Whitney JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 2021
- [AD 2015-14-05](https://openairdocs.org/ad/2015-14-05): Cracking in the low-pressure turbine (LPT) shaft · Pratt & Whitney Division JT8D-217C and JT8D-219. Effective Aug 25, 2015
- [AD 2011-04-04](https://openairdocs.org/ad/2011-04-04): Critical life-limited parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 22, 2011
- [AD 2011-03-01](https://openairdocs.org/ad/2011-03-01): Critical life- limited parts · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 9 more. Effective Mar 4, 2011
- [AD 2010-21-17](https://openairdocs.org/ad/2010-21-17): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 3 more. Effective Nov 12, 2010
- [AD 97-17-04 R1](https://openairdocs.org/ad/97-17-04-R1): Front compressor front hub · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Apr 22, 2010
- [AD 2009-24-01](https://openairdocs.org/ad/2009-24-01): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 5 more. Effective Jan 4, 2010
- [AD 2006-17-07 R1](https://openairdocs.org/ad/2006-17-07-R1): High pressure compressor (HPC) front hubs and HPC disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Nov 2, 2006
- [AD 2005-21-01](https://openairdocs.org/ad/2005-21-01): High pressure turbine (HPT) shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 21, 2005
- [AD 2005-17-16](https://openairdocs.org/ad/2005-17-16): Critical life-limited rotating parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Sep 30, 2005
- [AD 2004-26-04](https://openairdocs.org/ad/2004-26-04): HPT containment hardware · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 9, 2005
- [AD 2003-16-05](https://openairdocs.org/ad/2003-16-05): High pressure compressor (HPC) disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 12, 2003
- [AD 2003-12-07](https://openairdocs.org/ad/2003-12-07): 12th Stage high pressure compressor · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jul 18, 2003
- [AD 2003-05-07](https://openairdocs.org/ad/2003-05-07): Low pressure compressor (LPC) · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 17, 2003
- [AD 2002-21-17](https://openairdocs.org/ad/2002-21-17): Fan duct and fan exit guide vane · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 29, 2002
- [AD 2002-16-08](https://openairdocs.org/ad/2002-16-08): Combustion Chamber Outer Case (CCOC) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 20, 2002
- [AD 2001-15-18](https://openairdocs.org/ad/2001-15-18): Stage Compressor Disks · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Sep 4, 2001
- [AD 2000-22-06](https://openairdocs.org/ad/2000-22-06): Main Fuel Pump · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Dec 4, 2000
- [AD 99-10-11](https://openairdocs.org/ad/99-10-11): Fan Blades and Shrouds · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jun 14, 1999
- [AD 99-01-08](https://openairdocs.org/ad/99-01-08): Stage 7 through Stage 15 High-Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT3D-1, JT3D-1-MC6, JT3D-1-MC7 and 30 more. Effective Jan 5, 1999
- [AD 98-21-24](https://openairdocs.org/ad/98-21-24): Compressor Disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Nov 16, 1998
- [AD 98-04-39](https://openairdocs.org/ad/98-04-39): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Feb 25, 1998
- [AD 97-19-12](https://openairdocs.org/ad/97-19-12): Hub Inspection · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Nov 18, 1997
- [AD 97-19-14](https://openairdocs.org/ad/97-19-14): Low Pressure Turbine (LPT) Blade Sets · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Oct 24, 1997
- [AD 96-23-14](https://openairdocs.org/ad/96-23-14): Combustion Chamber Outer Cases · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 2, 1997
- [AD 96-15-06](https://openairdocs.org/ad/96-15-06): First Stage Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 3, 1996
- [AD 95-26-03](https://openairdocs.org/ad/95-26-03): High Pressure Compressor Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 11, 1996
- [AD 86-09-02 R2](https://openairdocs.org/ad/86-09-02-R2): Combustion Chamber Liners · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 17, 1995
- [AD 95-16-07](https://openairdocs.org/ad/95-16-07): High Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 11 more. Effective Sep 11, 1995
- [AD 95-10-10](https://openairdocs.org/ad/95-10-10): Compressor Fan Hub · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jul 21, 1995
- [AD 94-25-07](https://openairdocs.org/ad/94-25-07): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Mar 30, 1995
- [AD 95-02-16](https://openairdocs.org/ad/95-02-16): Fuel Nozzle and Support Assembly · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Feb 21, 1995
- [AD 94-20-09](https://openairdocs.org/ad/94-20-09): Low Pressure Turbine Blade Sets · Pratt & Whitney Division JT8D-15A, JT8D-17A and JT8D-17AR. Effective Nov 14, 1994
- [AD 91-24-14](https://openairdocs.org/ad/91-24-14): Bearing Seal Spacer · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jan 21, 1992
- [AD 89-25-11](https://openairdocs.org/ad/89-25-11): Fan Blade Retaining Plates · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jan 15, 1990
- [AD 89-24-02](https://openairdocs.org/ad/89-24-02): Fan Disk · Pratt & Whitney Division JT8D-7, JT8D-7A and JT8D-7B. Effective Nov 13, 1989
- [AD 88-04-02](https://openairdocs.org/ad/88-04-02): Anti-rotation Pin Failures · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 4, 1988
- [AD 87-03-13](https://openairdocs.org/ad/87-03-13): Compressor Blade · Pratt & Whitney Division JT8D-209, JT8D-217 and JT8D-217A. Effective Feb 16, 1987
- [AD 86-08-04 R1](https://openairdocs.org/ad/86-08-04-R1): HPC Removable Sleeve Spacers · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 4, 1986
- [AD 86-02-52 R1](https://openairdocs.org/ad/86-02-52-R1): Combustion Chamber · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 14, 1986
- [AD 85-19-51 R1](https://openairdocs.org/ad/85-19-51-R1): Second Stage Turbine Disk · Pratt & Whitney Division JT8D-15, JT8D-17 and JT8D-17R. Effective Dec 26, 1985
- [AD 78-17-02 R3](https://openairdocs.org/ad/78-17-02-R3): Compressor Front Hubs · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Mar 30, 1984
- [AD 80-15-51](https://openairdocs.org/ad/80-15-51): Engine Rear Compressor Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-1, JT8D-11 and 11 more. Effective Aug 21, 1980
- [AD 78-23-12](https://openairdocs.org/ad/78-23-12): Third Stage Turbine Blade Rivet · Pratt & Whitney Division JT8D-1, JT8D-1A, JT8D-1B and 5 more. Effective Dec 20, 1978
- [AD 77-16-12](https://openairdocs.org/ad/77-16-12): Low Turbine Shaft · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Aug 31, 1977
- [AD 76-24-01](https://openairdocs.org/ad/76-24-01): Eighth Stage Compressor Disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-1A and 6 more. Effective Jun 22, 1977
- [AD 77-07-11](https://openairdocs.org/ad/77-07-11): Fourth Stage Turbine Stator And Rotor · Pratt & Whitney Division JT8D-9 and JT8D-9A. Effective Apr 15, 1977
- [AD 77-03-06](https://openairdocs.org/ad/77-03-06): Compressor Front Hubs · Pratt & Whitney Division JT8D-1, JT8D-1A, JT8D-1B and 3 more. Effective Feb 25, 1977
- [AD 75-05-06](https://openairdocs.org/ad/75-05-06): Fuel Manifold Leakage · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Feb 24, 1977
- [AD 76-20-02](https://openairdocs.org/ad/76-20-02): Second Stage Fan Blades · Pratt & Whitney Division JT8D-1, JT8D-1A, JT8D-1B and 3 more. Effective Oct 10, 1976

### Historical (superseded or no longer in force)

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2016-07-28](https://openairdocs.org/ad/2016-07-28) (historical): Wings · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective Apr 26, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2012-18-05](https://openairdocs.org/ad/2012-18-05) (historical): Fuel · Boeing DC-9-11, DC-9-12, DC-9-13 and 21 more. Effective Oct 11, 2012
- [AD 2009-15-16](https://openairdocs.org/ad/2009-15-16) (historical): Doors · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 18 more. Effective Jul 6, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2007-10-04](https://openairdocs.org/ad/2007-10-04) (historical): Horizontal stabilizer · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 2 more. Effective May 23, 2007
- [AD 2006-07-25](https://openairdocs.org/ad/2006-07-25) (historical): Rudder pedal bracket · McDonnell Douglas DC-8-11, DC-8-12, DC-8-21 and 44 more. Effective May 16, 2006
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-06-16](https://openairdocs.org/ad/2001-06-16) (historical): AFM - Ice On Wing Upper Surfaces · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective May 7, 2001
- [AD 2001-07-10](https://openairdocs.org/ad/2001-07-10) (historical): Airplane Flight Manual - Landing Field Length · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Apr 27, 2001
- [AD 2000-15-17](https://openairdocs.org/ad/2000-15-17) (historical): Hydraulic Pipe Assembly in the Aft Fuselage · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Sep 12, 2000
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 99-24-04](https://openairdocs.org/ad/99-24-04) (historical): Hi-Lok Pin Fasteners · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Dec 27, 1999
- [AD 99-13-07](https://openairdocs.org/ad/99-13-07) (historical): Main Landing Gear Shock Strut Pistons · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 3 more. Effective Jul 28, 1999
- [AD 97-02-10](https://openairdocs.org/ad/97-02-10) (historical): Upper Lock Link Assembly Of Nose Landing Gear · McDonnell Douglas DC-9-80 Series (all), DC-9 Series (all), MD-88 and 1 more. Effective Feb 11, 1997
- [AD 96-19-09](https://openairdocs.org/ad/96-19-09) (historical): Main Landing Gear Pistons · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Oct 21, 1996
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 96-02-05](https://openairdocs.org/ad/96-02-05) (historical): Rudder Pedals Adjuster Hub Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Mar 25, 1996
- [AD 96-01-09](https://openairdocs.org/ad/96-01-09) (historical): Main Landing Gear Hydraulic Brake System · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Feb 26, 1996
- [AD 95-22-06](https://openairdocs.org/ad/95-22-06) (historical): Main Landing Gear Shock Strut Cylinder · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Nov 8, 1995
- [AD 95-19-09](https://openairdocs.org/ad/95-19-09) (historical): Inspect Sidewall Lighting · McDonnell Douglas DC-9-80 Series (all) and MD-88. Effective Oct 5, 1995
- [AD 95-12-25](https://openairdocs.org/ad/95-12-25) (historical): FIREX Pipe Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Jul 24, 1995
- [AD 95-09-10](https://openairdocs.org/ad/95-09-10) (historical): Wire Bundle In Overhead Switch Panel · McDonnell Douglas DC-9-80 Series (all) and MD-88. Effective May 19, 1995
- [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995
- [AD 92-27-07](https://openairdocs.org/ad/92-27-07) (historical): Rudder Pedals Adjuster Hub Assembly · McDonnell Douglas DC-9-11, DC-9-12, DC-9-13 and 20 more. Effective Jan 22, 1993
- [AD 92-03-02](https://openairdocs.org/ad/92-03-02) (historical): AFM Limitations Revision · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Jan 17, 1992
- [AD 91-21-11](https://openairdocs.org/ad/91-21-11) (historical): Slat Drive Mechanism Brackets · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Oct 30, 1991
- [AD 90-18-03](https://openairdocs.org/ad/90-18-03) (historical): Structural Failure · McDonnell Douglas DC-9-80 Series (all), DC-9 Series (all) and MD-88. Effective Sep 24, 1990
- [AD 89-14-02](https://openairdocs.org/ad/89-14-02) (historical): Rudder Pedal Bracket · McDonnell Douglas DC-8 Series (all), DC-9-80 Series (all), DC-9 Series (all) and 1 more. Effective Jul 5, 1989
- [AD 88-20-05](https://openairdocs.org/ad/88-20-05) (historical): Generator Power Feeder Cable · McDonnell Douglas DC-9-81, DC-9-82, DC-9-83 and 2 more. Effective Oct 31, 1988
- [AD 2011-07-02](https://openairdocs.org/ad/2011-07-02) (historical): Turbine Blade · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 28, 2011
- [AD 2006-17-07](https://openairdocs.org/ad/2006-17-07) (historical): Fretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 18 more. Effective Oct 4, 2006
- [AD 2005-18-02](https://openairdocs.org/ad/2005-18-02) (historical): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 28, 2006
- [AD 2005-02-03](https://openairdocs.org/ad/2005-02-03) (historical): Turbine (LPT) Blades 3rd and 4th Stage · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 3, 2005
- [AD 2002-23-14](https://openairdocs.org/ad/2002-23-14) (historical): High Pressure Compressor (HPC) Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 31, 2002
- [AD 2002-13-09](https://openairdocs.org/ad/2002-13-09) (historical): Rotating engine parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 30, 2002
- [AD 2000-21-07](https://openairdocs.org/ad/2000-21-07) (historical): Critical Life-Limited Parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 23, 2001
- [AD 99-26-06](https://openairdocs.org/ad/99-26-06) (historical): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 22, 2000
- [AD 99-27-01](https://openairdocs.org/ad/99-27-01) (historical): Low Pressure Turbine Blades · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 2, 2000
- [AD 99-22-14](https://openairdocs.org/ad/99-22-14) (historical): High Pressure Turbine Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 1999
- [AD 99-12-04](https://openairdocs.org/ad/99-12-04) (historical): Critical Life Limited Part Inspection · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jul 8, 1999
- [AD 97-19-13](https://openairdocs.org/ad/97-19-13) (historical): High Pressure Turbine (HPT) Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Oct 24, 1997
- [AD 97-17-04](https://openairdocs.org/ad/97-17-04) (historical): Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Sep 30, 1997

All 262: https://openairdocs.org/aircraft/N997DL/ads.md

## Information bulletins (advisory) (12 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-08-43](https://openairdocs.org/saib/NM-08-43): Cabin Equipment/Furnishings - Seats. Issued Sep 3, 2008
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006
- [SAIB NE-16-22](https://openairdocs.org/saib/NE-16-22): Turbine Engine Combustion Section  JT8D Series Turbofan Engines. Issued Sep 2, 2016
- [SAIB NE-10-32](https://openairdocs.org/saib/NE-10-32): Turbine Engine Accessory Drive. Issued May 7, 2010
- [SAIB NE-05-75R1](https://openairdocs.org/saib/NE-05-75R1): . Issued Aug 4, 2005
- [SAIB NE-05-30](https://openairdocs.org/saib/NE-05-30): . Issued Feb 3, 2005
- [SAIB NE-02-22](https://openairdocs.org/saib/NE-02-22): . Issued Mar 26, 2002
- [SAIB NE-02-08R1](https://openairdocs.org/saib/NE-02-08R1): . Issued Feb 8, 2002
- [SAIB NE-01-42](https://openairdocs.org/saib/NE-01-42): . Issued Sep 25, 2001
- [SAIB ANE-97-03](https://openairdocs.org/saib/ANE-97-03): . Issued Apr 25, 1997
- [SAIB NE-05-75](https://openairdocs.org/saib/NE-05-75) (historical): . Issued Jul 22, 2005

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC99LA023](https://openairdocs.org/ntsb/NYC99LA023), Oct 11, 1998: McDonnell Douglas MD-88 (N997DL), Covington, KY, substantial damage. Probable cause: The tug driver's failure to maintain a proper visual lookout.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19980314033769I](https://openairdocs.org/incident/19980314033769I), Mar 14, 1998: Doug MD88 (N997DL), Portland, ME, Minor damage. At 1310 local time on March 14, 1998, a delta airlines, MD-88, N997DL was completing a routine passenger flight (flt #2158) from cincinnati, oh (cvg) to…

## Service difficulty reports (244, newest 50)

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

- [SDR DALA2020040202117](https://openairdocs.org/sdr/DALA2020040202117), Apr 1, 2020: HOOK AND LOOP. FAULTY. DURING THE FUNCTIONAL CHECK THE TAIL CONE SLIDE DID NOT ROLL OUT AND DEPLOY AS DESIGNED. MAINTENANCE FOUND FAULTY VELCRO ON THE LANYARD. REPLACE BOTH THE VELCRO
- [SDR DALA2020032301989](https://openairdocs.org/sdr/DALA2020032301989), Mar 23, 2020: OIL SYSTEM. UNKNOWN. AFTER T/O, FLT ATTND CALLED AND NOTIFIED THE FLT DECK OF BURNING ELECTRICAL SMELL FROM REAR JUMP SEAT AREA. FLT DECK AREA HAD A SLIGHT ODOR OF BURNING OIL BUT D
- [SDR DALA2020031801916](https://openairdocs.org/sdr/DALA2020031801916), Mar 18, 2020: BATTERY. DISCHARGED. OVERWING EMERGENCY EXIT LIGHTS INOP AT ROW 25. REPL BATTERIES PER MD88 AMM 33-53. OPS CHECK GOOD. (LP6104945)
- [SDR DALA2020011400245](https://openairdocs.org/sdr/DALA2020011400245), Jan 13, 2020: WINDSHIELD WIPER. DETACHED. CAPT SIDE WIPER ARM DEPARTED AIRCRAFT ON DESCENT. REP CAPT WINDSHIELD WIPER REF MD 88 M/M 30-42. (LP5498940)
- [SDR DALA2019102706184](https://openairdocs.org/sdr/DALA2019102706184), Oct 26, 2019: STATIC PORT. LEAKING. SDR REPORTED DUE TO DECLARED EMERGENCY PER MCC REPORT. AFTER TAKEOFF, AIRSPEED ERRATIC. DISCONNECTED AUTOPILOT + AUTOTHROTTLES. RECEIVED VECTORS FROM ATL. CONFI
- [SDR DALA2019091605321](https://openairdocs.org/sdr/DALA2019091605321), Sep 15, 2019: FITTING. CRACKED. UPPER LT FITTING ON TAILCONE CRACKED. REMOVED UPPER LT TAILCONE FITTING. REPLACED UPPER LT FITTING ANGLE PER SRM 53-54-0 PAGE 3. OK FOR SERVICE. (LP1272698)
- [SDR DALA2019091605320](https://openairdocs.org/sdr/DALA2019091605320), Sep 15, 2019: BEARING. EXCESS PLAY. TAIL CONE RELEASE HAS PLAY AND IS CONTACTING THE FRAME. REMOVED TAIL CONE MECHANISM PER AMM 53-53-02. 542402. REPLACED RELEASE CAM BEARING IAW CMM 53-50-07. REI
- [SDR DALA2019091605319](https://openairdocs.org/sdr/DALA2019091605319), Sep 15, 2019: FRAME. CRACKED. TAILCONE ATTACH FRAME CRACKED @2:00 POSITION AT PIN. REMOVED FRAME P/N 9911843-6. DRILLED UP REPLACEMENT FRAME P/N 5966769U501 PER DWG 9911843. (458779) INSTALL
- [SDR DALA2019090805202](https://openairdocs.org/sdr/DALA2019090805202), Sep 5, 2019: FRAME. CRACKED. RT FWD MAIN LANDING GEAR WHEEL FRAME CRACK. INSTALLED NEW RT FWD MLG W/W FRAME SECTION REF ERA 581127-14 REV 0 PERMANENT REPAIR. (LP6026692)
- [SDR DALA2019050302804](https://openairdocs.org/sdr/DALA2019050302804), May 2, 2019: STRUCTURE. CRACKED. CRUISING AT FL 320 FLOW LIGHT CAME ON. OUTFLOW VALVE FULLY CLOSED. DESCENDED NORMALLY. FLOW LIGHT EXTINGUISHED AT APPROXIMATELY FL240. TIGHTEN FITTING FOR RT PI
- [SDR DALA2019042202548](https://openairdocs.org/sdr/DALA2019042202548), Apr 21, 2019: SKIN. CORRODED. ON WALK AROUND FOUND CORROSION LWR FWD CORNER OF AFT LAV SERVICE DOOR AREA. C/W REPAIR PER ERA 577463-14 REV ORIG - ALL RII ITEMS C/W. (LP5673084)
- [SDR DALA2019031101555](https://openairdocs.org/sdr/DALA2019031101555), Mar 11, 2019: LIGHT. INOPERATIVE. 3C SEAT EMERGENCY LIGHT INOP. RELAMPED BULBS. LIGHTS CKS OK AT 3C. REF MM 33-53. (LP5832911)
- [SDR DALA2019031101554](https://openairdocs.org/sdr/DALA2019031101554), Mar 11, 2019: BATTERY. DISCHARGED. ROW 25 EMERGENCY EXIT SIGN INOP BOTH SIDES. R+R BATTERIES FOR BATTERY PACK IAW MM 33-53. LIGHT CKS OK. (LP5832910)
- [SDR DALA2018100305854](https://openairdocs.org/sdr/DALA2018100305854), Sep 18, 2018: HYDRAULIC LINE. LEAKING. SHIP 997 ON FLIGHT 296 FROM ATL TO RDU DECLARED AN EMERGENCY DUE TO AN EOAP LOW RIGHT HYDRAULIC SYSTEM QUANTITY MESSAGE. CORRECTIVE ACTION: RDU MAINTENANCE FOUN
- [SDR DALA2018090705491](https://openairdocs.org/sdr/DALA2018090705491), Sep 4, 2018: FASTENER. MISSING. FASTENERS MISSING FROM LT AILERON CLOSEOUT PANEL. INSTALLED FASTENERS. OK FOR SVC. SDR REPORTED DUE TO THE FACT THAT THE FASTENERS COULD HAVE DEPARTED THE AIRCR
- [SDR DALA2018080804932](https://openairdocs.org/sdr/DALA2018080804932), Aug 6, 2018: LENS. MISSING. RIGHT POSITION LIGHT LENS WAS MISSING. REMOVED AND REPLACED THE RT POSITION LIGHT ASSY IAW AMM 33-43, OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR DALA2018060803885](https://openairdocs.org/sdr/DALA2018060803885), Jun 6, 2018: BATTERY PACK. NO TEST. FAILED EMERGENCY LIGHT BATTERY PACK AT BS 1338. THE BATTERY PACK WAS REPLACED IAW AMM 33-53-00. OPS TESTED GOOD IAW AMM 33-53-00.
- [SDR DALA2018060763862](https://openairdocs.org/sdr/DALA2018060763862), Jun 5, 2018: SCREW. OUT OF TOLERANCE. DURING A HORIZONTAL STABILIZER ACTUATOR ASSEMBLY END PLAY CHECK, THE FINAL END PLAY READ MORE THAN 0.040 INCH. SCREW AND NUT WERE REMOVED AND REPLACED IAW AMM 2
- [SDR DALA2018060603841](https://openairdocs.org/sdr/DALA2018060603841), Jun 5, 2018: CHANNEL. CRACKED. A CRACKED AFT CHANNEL, ON THE FWD RT MLG WW DOOR FRAME BS 937, RBL 55. THE CHANNEL WAS REPLACED IAW SRM 51-30-02, AND SRM 51-30-05.
- [SDR DALA2018060103747](https://openairdocs.org/sdr/DALA2018060103747), May 31, 2018: FLOOR PANEL. DELAMINATED. FLOOR PANEL 693C DELAMINATED AT AFT END. THE FLOOR PANEL WAS REPLACED IAW AMM. 53-20-01-201.
- [SDR DALA2018051203243](https://openairdocs.org/sdr/DALA2018051203243), May 11, 2018: DUCT. DAMAGED. APU FAILED INFLIGHT LEFT GEN DEFERRED. EMERGENCY WAS DECLARED. FOUND APU SURGE VALVE DUCT DAMAGE. R&R SURGE VALVE DUCT PER AMM 49-50. R&R NR 1 ENG GENERATOR DRI
- [SDR DALA2018032601879](https://openairdocs.org/sdr/DALA2018032601879), Mar 26, 2018: LAMP. INOPERATIVE. SEAT ROW 23 RT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. SYSTEM CHECKED GOOD.
- [SDR DALA2018011200224](https://openairdocs.org/sdr/DALA2018011200224), Jan 11, 2018: BATTERY PACK. DISCHARGED. OVERWING EMERGENCY LIGHT INOP. T/S, R&R OVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK PER MM 33-53. OPS CHK - GOOD. OK FOR SVC.
- [SDR DALA2017122608874](https://openairdocs.org/sdr/DALA2017122608874), Dec 24, 2017: BATTERY PACK. FAILED. OVERHEAD EMERGENCY LIGHTS AT ROWS 10 AND 13 INOPERATIVE. FOUND THE BATTERIES BAD AT SEAT ROWS 10 THRU 13 AND REPLACED IAW SPWM 20 AND EWIS. OPS CK GOOD.
- [SDR DALA2017122608848](https://openairdocs.org/sdr/DALA2017122608848), Dec 24, 2017: WIRE HARNESS. FAILED. EMERGENCY LIGHTS AT SEATS 18 AND 22 DE INOPERATIVE. REPLACED THE EMERGENCY LIGHT HARNESSES AT SEATS 18 AND 22 DE. OPS CHECKED GOOD IAW SPWM 20 AND EWIS.
- [SDR DALA2017112608287](https://openairdocs.org/sdr/DALA2017112608287), Nov 24, 2017: WIRE HARNESS. DAMAGED. SEAT 13ED EMERGENCY LIGHT INOPERATIVE. FOUND THE WIRES PULLED FROM THE CONNECTOR. REPLACED THE WIRE HARNESS. OPS CHECKED GOOD IAW AMM33-52.
- [SDR DALA2017102407750](https://openairdocs.org/sdr/DALA2017102407750), Oct 24, 2017: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 1407, LONGERON 2L. COMPLIED WITH PRI 540097-14AD REV C REV 0.
- [SDR DALA2017072505692](https://openairdocs.org/sdr/DALA2017072505692), Jul 23, 2017: DOUBLER. DAMAGED. NR 2 PYLON HYD SUPPLY HOSE FITTING LOOSE IN FIREWALL. REMOVED ORIGINAL REPAIR. FABRICATED REPAIR DOUBLER PER RI 560468-14. CLEANED UP HYD PRESSURE LINE HOLE IAW
- [SDR DALA2016112809375](https://openairdocs.org/sdr/DALA2016112809375), Nov 27, 2016: ENGINE. FAILED. RETURNED TO DEPARTURE DUE TO RIGHT ENGINE ISSUES. THE CREW REPORTED THAT ON TAKEOFF AT FL50 THE NR 2 ENGINE LOST OIL PRESSURE, HYDRAULICS AND STARTED VIBRATING.
- [SDR DALA2016112809293](https://openairdocs.org/sdr/DALA2016112809293), Nov 27, 2016: ENGINE. FAILED. AFTER TAKEOFF, APPROACHING 5000 MSL, LOST OIL PRESSURE AND RIGHT ENGINE HAD SEVERE VIBRATIONS, LOSS OF RIGHT HYDRAULIC SYSTEM. VIBRATIONS STILL PRESENT ON WINDM
- [SDR DALA2016062004777](https://openairdocs.org/sdr/DALA2016062004777), Jun 18, 2016: BATTERY. DISCHARGED. DURING SERVICE CHECK, FOUND COCKPIT, R1, L1 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY POWER PACK BATTERIES IAW AMM 33-50. OPS CHECK GOOD.
- [SDR DALA2016050903804](https://openairdocs.org/sdr/DALA2016050903804), May 8, 2016: ACCESS PANEL. CORRODED. CORROSION AND WEAR ON SEATING AREA OF SECONDARY ACCESS PANELS, 1409C, 1410C AT RT WING. HEATER BLANKET WAS REPLACED IAW AMM 30-80-02, PAGE BLOOCK 401.
- [SDR DALA2016050903803](https://openairdocs.org/sdr/DALA2016050903803), May 8, 2016: ACCESS PANEL. CORRODED. CORROSION ON SEATING AREA OF SECONDARY ACCESS PANELS, 1303C, 1307C AT LT WING. HEATER BLANKET WAS REPLACED IAW AMM 30-80-02, PAGEBLOCK 401.
- [SDR DALA2016050903807](https://openairdocs.org/sdr/DALA2016050903807), May 7, 2016: LANYARD. TORN. MAINTENANCE FOUND THE TAILCONE LANYARD TORN. THE LANYARD WAS REPLACED.
- [SDR DALA2016050803802](https://openairdocs.org/sdr/DALA2016050803802), May 7, 2016: BEAM. CRACKED. CRACKED VENTRAL STAIR BEAM 1485 X=10 AT AAC. CRACKED BEAM WAS ATTENDED WITH SRM 51-10-4, 51-10-3, 51-30-1, 51-30-2 AND 51-30-5.
- [SDR DALA2016050603707](https://openairdocs.org/sdr/DALA2016050603707), May 5, 2016: DOOR FRAME. CRACKED. CRACKED NLG DOOR JAMB, LT SIDE. LT JAMB AND LT STEP WERE REMOVED IAW SRM 51-30-2 AND SRM 51-30-5. REPAIR WAS ACCOMPLISHED IAW ER/A NR 545103-14 AND ETI-88-16-14
- [SDR DALA2016050603704](https://openairdocs.org/sdr/DALA2016050603704), May 5, 2016: BUSHING. CORRODED. CORROSION FOUND ON BUSHINGS AT RT OVERWING HEATER BLANKET REAR SPAR. BUSHINGS 1, 2, 6, 7, 8, 9 AND 10 WERE REPLACED IAW SRM 51-30-10 AND BUSHINGS 3, 4 AND 5 WER
- [SDR DALA2016050603703](https://openairdocs.org/sdr/DALA2016050603703), May 5, 2016: LONGERON. CRACKED. CRACKED LONGERON 15 RT AT CENTER WING FUEL TANK BS XEW 12. REPAIR WAS ACOMPLISHED IAW ETI-88-16-143, REV 3 AND ETI-88-16-145, REV ORIGINAL AND ER/A 545092-14, R
- [SDR DALA2016050603696](https://openairdocs.org/sdr/DALA2016050603696), May 4, 2016: ANGLE. CORRODED. CORROSION UNDER LOWER R1 DOOR JAMB FLOOR LEVEL CUSP ANGLE RBL 60, BS 196. CUSP ANGLE WAS REPAIRED IAW SRM 53-05, FIG 55 AND ETI-88-16-153, REV 5, ER/A 545109-14
- [SDR DALA2016050503643](https://openairdocs.org/sdr/DALA2016050503643), May 4, 2016: CARGO TRACK. CORRODED. CORROSION ON LT CARGO TRACK FROM BS 1155 TO 1222 IN THE AFT CARGO BAY. CARGO TRACK WAS REPAIRED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4 AND 51-10-3, PAR 14, 
- [SDR DALA2016050503639](https://openairdocs.org/sdr/DALA2016050503639), May 4, 2016: FRAME. CRACKED. CRACKED FRAME CLIPS 1437 BETWEEN LONGERON 1RT AND 3RT. FRAME CLIPS WERE REPLACED IAW DOUGLAS DWG NR 9953016, REV AT, ETI-88-16-191 REV 1 AND ER/A 545160-14, REV
- [SDR DALA2016050403616](https://openairdocs.org/sdr/DALA2016050403616), May 3, 2016: SKIN. PUNCTURED. PUNCTURED LOWER SURFACE COVER ON INBD VANE OTBD FLAP XV1=211 AT LT WING. REPAIR FABRICATED IAW SRM 57-01, FIG 3. REPAIR TREATED AND PAINTED IAW SRM 51-10-3, PAR
- [SDR DALA2016050403614](https://openairdocs.org/sdr/DALA2016050403614), May 3, 2016: SKIN. CRACKED. CRACKED FUSELAGE SKIN 1419 BETWEEN LONG 1 AND 2 RT AT AAC. AREA WAS REPAIRED I IAW ETI-88-16-152, REV. 1 AND ER/A 545106-14AD REV ORIGINAL.
- [SDR DALA2016050203518](https://openairdocs.org/sdr/DALA2016050203518), May 1, 2016: SKIN. WORN. WORN PREVIOUS DOUBLER REPAIR ON FWD FUSELAGE SKIN BS 133 LONG 15L AT FWD FUSELAGE. REPAIRED IAW ETI-88-16-187, REV 1 AND ER/A 545154-14, REV ORIGINAL.
- [SDR DALA2016050203514](https://openairdocs.org/sdr/DALA2016050203514), May 1, 2016: FLOOR SUPPORT. DAMAGED. ELONGATED HOLES ON FLOOR SUPPORT MID CARGO COMPARTMENT BETWEEN BS 769 TO 786.5 AND LONGERON 27R-28R. ETI-88-16-146 WAS ACCOMPLISHED ON PN 5936594-529 LT AND PN 
- [SDR DALA2016050203519](https://openairdocs.org/sdr/DALA2016050203519), Apr 30, 2016: FRAME. CORRODED. CORROSION ON FRAME BS 1271 BETWEEN LONGERON 30 AND 29 LT AT AFT CARGO COMPARTMENT. FRAME WAS REPAIR IAW SRM 53-03, FIG 2A AND 51-10-3 P14, 16, 51-30-5, 51-30-2.
- [SDR DALA2016050203506](https://openairdocs.org/sdr/DALA2016050203506), Apr 30, 2016: DOUBLER. CORRODED. CORROSION ON PREVIOUS REPAIR DOUBLER AT MID CARGO DOOR JAMB. NEW SPACER WAS FABRICATED AND TREATED, PAINTED, WAS INSTALLED IAW SRM 53-05, FIG 123, 51-10-3 PAR 2
- [SDR DALA2016050103503](https://openairdocs.org/sdr/DALA2016050103503), Apr 30, 2016: SKIN. CORRODED. CORROSION ON BARRIEL NUTS NR 13, 20 AND 25 XH -27. CORROSION ON BARRIEL NUTS NR 13, 20 AND 25 XH =-27 WAS REPAIRED IAW ERA NR 545115-14, REV: ORIGINAL.
- [SDR DALA2016050103500](https://openairdocs.org/sdr/DALA2016050103500), Apr 30, 2016: FRAME. CRACKED. CRACK ON FRAME WEB BS 1485 BELOW VENTRAL ACTUATOR FITTING. FRAME WEB WAS REPAIRED IAW SRM 51-01, PAR 21, 53-03 FIG 43, 51-30-2 AND 51-30-5.
- [SDR DALA2016043003497](https://openairdocs.org/sdr/DALA2016043003497), Apr 29, 2016: ACCESS PANEL. UNKNOWN. PERFORM SERVICE TO FUEL TANK ACCESS PLATES ON RT WING. SERVICE ON ACCESS NR 1476C, 2302C, 1478C, 1464C AND 1466C WERE PERFORMED AND ACCESS NRS 1410C, 1436C,1472

All 244: https://openairdocs.org/aircraft/N997DL/reports.md

## STCs that may be installed (OpenAirDocs) (265, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Mcdonnell Douglas MD-88)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03184AT-D](https://openairdocs.org/stc/ST03184AT-D): Interior modification. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03849AT-D](https://openairdocs.org/stc/ST03849AT-D): Installation of an Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03990AT](https://openairdocs.org/stc/ST03990AT): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST04752NY](https://openairdocs.org/stc/ST04752NY): Replacement of Dual Analog Radio Altimeter Transceivers with Dual 5G Tolerant Collins Aerospace or Honeywell Digital Radio Altimeters Transceivers and Dual Shadin Digital-to-Analog Converters. S. LB Aircraft Engineering
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST09180AC](https://openairdocs.org/stc/ST09180AC): Installation of DeVore Wing Forward Position Lights. The Boeing Company
- [STC ST09181AC](https://openairdocs.org/stc/ST09181AC): Installation of main landing gear spotlights. The Boeing Company
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA5786NM](https://openairdocs.org/stc/SA5786NM): Installation of an overhead life raft stowage compartment kit. Safran Cabin Inc
- [STC SA7079NM](https://openairdocs.org/stc/SA7079NM): Installation C&D Interiors passenger service units, overhead storage units, sidewall panels, and ceiling panels. Safran Cabin Inc
- [STC ST00588LA](https://openairdocs.org/stc/ST00588LA): Installation of galleys G1 and G2. Safran Cabin Inc
- [STC ST00687LA](https://openairdocs.org/stc/ST00687LA): Installation of Interior Kit. Safran Cabin Inc
- [STC ST00873SE](https://openairdocs.org/stc/ST00873SE): Installation of ESCI SX I Interior Retrofit Kit. Safran Cabin Inc
- [STC ST00879SE](https://openairdocs.org/stc/ST00879SE): Installation of ESCI SX II Interior Retrofit Kit. Safran Cabin Inc
- [STC ST00943LA](https://openairdocs.org/stc/ST00943LA): Installation of bin extension assembly. Safran Cabin Inc
- [STC ST00975LA](https://openairdocs.org/stc/ST00975LA): Installation of bin extension assembly. Safran Cabin Inc
- [STC ST01336LA](https://openairdocs.org/stc/ST01336LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01993LA-D](https://openairdocs.org/stc/ST01993LA-D): Interior Installations. Safran Cabin Inc
- [STC SA3165NM](https://openairdocs.org/stc/SA3165NM): Installation of Floor Proximity Emergency Escape Path Marking System. Bruce Aerospace Inc
- [STC ST00092LA](https://openairdocs.org/stc/ST00092LA): Instalation of interior fluorescent cabin lighting system. Bruce Aerospace Inc
- [STC ST01554AT](https://openairdocs.org/stc/ST01554AT): Increasing data recording parameters to 17/18 parameters on digital flight data recorders (DFDR), for L-3 Com (formerly Loral/Fairchild) DFDR, and Allied Signal DFDR part numbers identified by this STC,. Acron Aviation Inc
- [STC ST03560AT](https://openairdocs.org/stc/ST03560AT): Installation of L3 Communications Aviation Recorders Micro Quick Access Recorder (uQAR) o. Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01818CH](https://openairdocs.org/stc/ST01818CH): Installation of a Honeywell Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01887CH](https://openairdocs.org/stc/ST01887CH): Installation of GPS antenna provisions. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02316CH](https://openairdocs.org/stc/ST02316CH): Upgrade of existing Mode S transponder installation to add enhanced surveillance Mode S. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02474AK](https://openairdocs.org/stc/ST02474AK): Installation of escape tapes at the L1 and R1 entry doors and removal of evacuation slides. Tatonduk Outfitters Ltd
- [STC ST02770SE](https://openairdocs.org/stc/ST02770SE): Installation of an Improved Radio Altimeter System. AeroMech Incorporated
- [STC ST01987AT](https://openairdocs.org/stc/ST01987AT): Installation of STG Aerospace Inc. photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST02928AT](https://openairdocs.org/stc/ST02928AT): Installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS). Woven Electronics LLC
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST02761AT](https://openairdocs.org/stc/ST02761AT): Installation of Honeywell RESCU 406AF Emergency Locator Transmitter (ELT). Woven Electronics, LLC
- [STC SA4200NM-D](https://openairdocs.org/stc/SA4200NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC SA9024NM-D](https://openairdocs.org/stc/SA9024NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC ST03276AT](https://openairdocs.org/stc/ST03276AT): Installation of a Honeywell MK II Aircraft Communications Addressing and Reporting System (ACARS). Woven Electronics, LLC
- [STC ST02896AT](https://openairdocs.org/stc/ST02896AT): Installation of a Kannad Model 406-AF Emergency Locator Transmittter (ELT). Woven Electronics LLC
- [STC ST01997CH](https://openairdocs.org/stc/ST01997CH): Installation of a Honeywell RESCU 406AF emergency locator transmitter (ELT) system. Honeywell International Inc
- [STC ST02372LA](https://openairdocs.org/stc/ST02372LA): Installation of modifications to improve the airplane cruise performance. Super98 LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST03824AT](https://openairdocs.org/stc/ST03824AT): Installation of an Universal Avionics Terrain Awareness and Warning Systems (TAWS). Technical Aero Services Inc
- [STC ST03831AT](https://openairdocs.org/stc/ST03831AT): Installation of an Universal Avionics EFI-640 Electronic Flight Instrument System (EFIS). Technical Aero Services Inc
- [STC ST03838AT](https://openairdocs.org/stc/ST03838AT): Installation of an Universal Avionics Application Server Unit (ASU) System Class II Electronic Flight Bag (EFB). Technical Aero Services Inc
- [STC SA2726SO](https://openairdocs.org/stc/SA2726SO): Installation of CAS-81 TCAS II system. Honeywell International Inc
- [STC SA2727SO](https://openairdocs.org/stc/SA2727SO): Installation of Dual TRA-67 Model S Transponder system. Honeywell International Inc
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation

All 265: https://openairdocs.org/aircraft/N997DL/stcs.md

## Related

- Other Mcdonnell Douglas MD-88 aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-88/aircraft.md
- The Pratt & Whitney JT8D series engine: https://openairdocs.org/engine/pratt-whitney-jt8d-series.md

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