# N929DN: 1996 Mcdonnell Douglas MD-90-30

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-90-30](https://openairdocs.org/model/mcdonnell-douglas-md-90-30) (registry code 3023690, 142 seats)
- Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 53459
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 17, 2011
- Certificate issued: December 18, 2015
- Expires: December 31, 2028
- Mode S code: ACDFF1
- Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=929DN
- Page: https://openairdocs.org/aircraft/N929DN

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.

## ADs that may apply (OpenAirDocs): 91 in force

### Matched by airframe (Mcdonnell Douglas MD-90-30)

- [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 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 2019-24-17](https://openairdocs.org/ad/2019-24-17): Wings · Boeing MD-90-30. Effective Jan 24, 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 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-11-02](https://openairdocs.org/ad/2017-11-02): Stabilizers · Boeing MD-90-30. Effective Jun 27, 2017
- [AD 2016-25-26](https://openairdocs.org/ad/2016-25-26): Navigation · Boeing MD-90-30. Effective Feb 2, 2017
- [AD 2016-22-18](https://openairdocs.org/ad/2016-22-18): Fuselage · Boeing MD-90-30. Effective Nov 21, 2016
- [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 2014-24-03](https://openairdocs.org/ad/2014-24-03): Stabilizers · Boeing MD-90-30. Effective Jan 27, 2015
- [AD 2014-24-04](https://openairdocs.org/ad/2014-24-04): Stabilizers · Boeing MD-90-30. Effective Jan 13, 2015
- [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 2012-22-04](https://openairdocs.org/ad/2012-22-04): Wings · Boeing MD-90-30. Effective Dec 5, 2012
- [AD 2012-21-18](https://openairdocs.org/ad/2012-21-18): Wings · Boeing MD-90-30. Effective Dec 5, 2012
- [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 2011-12-12](https://openairdocs.org/ad/2011-12-12): Stabilizers · Boeing MD-90-30. Effective Jul 22, 2011
- [AD 2011-06-12](https://openairdocs.org/ad/2011-06-12): Stabilizers · Boeing MD-90-30. Effective Apr 26, 2011
- [AD 2011-03-09](https://openairdocs.org/ad/2011-03-09): Ignition · Boeing MD-90-30. Effective Mar 14, 2011
- [AD 2011-01-11](https://openairdocs.org/ad/2011-01-11): Stabilizers · Boeing MD-90-30. Effective Feb 9, 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 2010-22-04](https://openairdocs.org/ad/2010-22-04): Nacelles/Pylons · Boeing MD-90-30. Effective Dec 3, 2010
- [AD 2010-21-16](https://openairdocs.org/ad/2010-21-16): Hydraulic Power · Boeing MD-90-30. Effective Nov 18, 2010
- [AD 2010-16-11](https://openairdocs.org/ad/2010-16-11): Wings · Boeing MD-90-30. Effective Sep 22, 2010
- [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 2010-05-04](https://openairdocs.org/ad/2010-05-04): Fuselage · Boeing MD-90-30. Effective Apr 1, 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 2009-13-08](https://openairdocs.org/ad/2009-13-08): Stabilizers · Boeing MD-90-30. Effective Aug 3, 2009
- [AD 2009-11-11](https://openairdocs.org/ad/2009-11-11): Fuel · Boeing MD-90-30. Effective Jul 7, 2009
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 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 2007-17-19](https://openairdocs.org/ad/2007-17-19): Static port heater assemblies · Boeing MD-90-30. Effective Oct 2, 2007
- [AD 2006-16-09](https://openairdocs.org/ad/2006-16-09): Refueling manifold in the right wing refueling station area · Boeing MD-90-30. Effective Sep 13, 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 2005-13-14](https://openairdocs.org/ad/2005-13-14): Dual anti-skid control manifolds (DACM) · Boeing MD-90-30. Effective Jul 29, 2005
- [AD 2005-09-08](https://openairdocs.org/ad/2005-09-08): Aft left lavatory · Boeing MD-90-30. Effective May 20, 2005
- [AD 2005-06-03](https://openairdocs.org/ad/2005-06-03): fluorescent light lamp holders · Boeing MD-90-30. Effective Apr 20, 2005
- [AD 2005-05-02](https://openairdocs.org/ad/2005-05-02): Electrical/electronics (E/E) compartment · Boeing MD-90-30. Effective Apr 6, 2005
- [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 2004-07-12](https://openairdocs.org/ad/2004-07-12): Terminal studs on the 3-phase limiter blocks · Boeing MD-90-30. Effective May 11, 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 2004-05-18](https://openairdocs.org/ad/2004-05-18): Main Landing Gear (MLG) · Boeing MD-90-30. Effective Apr 13, 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 2003-26-07](https://openairdocs.org/ad/2003-26-07): Circuit Breakers · Boeing MD-90-30. Effective Feb 4, 2004
- [AD 2003-11-15 R1](https://openairdocs.org/ad/2003-11-15-R1): Pressure relief door · Boeing MD-90-30. Effective Jan 27, 2004

### Matched by engine (IAE V2500SERIES)

None in force.

### 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 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 2009-07-04](https://openairdocs.org/ad/2009-07-04) (historical): Auxiliary hydraulic power system · McDonnell Douglas MD-90-30. Effective May 5, 2009
- [AD 2008-18-10](https://openairdocs.org/ad/2008-18-10) (historical): Aft mount support fitting · McDonnell Douglas MD-90-30. Effective Sep 24, 2008
- [AD 2005-03-05](https://openairdocs.org/ad/2005-03-05) (historical): Aft left lavatory · Boeing MD-90-30. Effective Feb 22, 2005
- [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 2003-11-15](https://openairdocs.org/ad/2003-11-15) (historical): Pressure relief door for the thrust reverser · McDonnell Douglas MD-90-30. Effective Jul 9, 2003
- [AD 2003-04-10](https://openairdocs.org/ad/2003-04-10) (historical): Wire Chafing · McDonnell Douglas MD-90-30. Effective Apr 4, 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 2001-07-10](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 2000-20-04](https://openairdocs.org/ad/2000-20-04) (historical): Electrical Power Control Unit (EPCU) · McDonnell Douglas MD-90-30. Effective Nov 13, 2000
- [AD 2000-16-01](https://openairdocs.org/ad/2000-16-01) (historical): Electrical Power Control Unit (EPCU) · McDonnell Douglas MD-90-30. Effective Sep 19, 2000
- [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 2000-03-08](https://openairdocs.org/ad/2000-03-08) (historical): Main Landing Gear (MLG) Piston · McDonnell Douglas MD-90-30. Effective Mar 22, 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 99-13-07](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 97-11-07](https://openairdocs.org/ad/97-11-07) (historical): Structural Integrity · Boeing MD-90-30. Effective Jun 26, 1997
- [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

All 112: https://openairdocs.org/aircraft/N929DN/ads.md

## Information bulletins (advisory) (4 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-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [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

## NTSB investigations

None matched to N929DN.

## FAA accident and incident reports

None matched to N929DN.

## Service difficulty reports (107, 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 DALA2018110106384](https://openairdocs.org/sdr/DALA2018110106384), Oct 31, 2018: FUEL NOZZLE. LEAKING. F/A IN AFT JUMPSEAT SAID SMELLED OILY / EXHAUST SMELL IN AFT CABIN DURING FLIGHT. NO SMOKE. SAID IT WENT AWAY AND CAME BACK IN DECENT. INSPECTED APU. FOUND LOWE
- [SDR DALA2018031301586](https://openairdocs.org/sdr/DALA2018031301586), Mar 13, 2018: ENGINE. FAILED. AIR TURNBACK DUE TO A NR 1 ENGINE COMPRESSOR STALL AND BLUE FLAMES COMING FROM THE ENGINE AFTER TAKE-OFF, DURING CLIMB AT 2,300 FEET. THE FLIGHT CREW FOLLOWED T
- [SDR DALA2018013000580](https://openairdocs.org/sdr/DALA2018013000580), Jan 30, 2018: LATCH. WORN. TAIL CONE UPPER LATCH IS WORN. REPLACED UPPER LEFT HAND LATCH IAW MM. OPERATION CHECKS GOOD.
- [SDR DALA2018013000579](https://openairdocs.org/sdr/DALA2018013000579), Jan 30, 2018: LIGHT. INOPERATIVE. TAIL CONE SLIDE LIGHTS DID NOT LIGHT UP ON DEPLOYMENT. SLIDE REPLACED ON CARD 251-4643.
- [SDR DALA2017103007893](https://openairdocs.org/sdr/DALA2017103007893), Oct 29, 2017: FITTING. BROKEN. INTERNAL RELEASE HANDLE CLIP BROKEN FOR TAIL CONE. CLIP REPLACED.
- [SDR DALA2017102907892](https://openairdocs.org/sdr/DALA2017102907892), Oct 28, 2017: STRUCTURE. CORRODED. CORROSION AT MID CARGO DOOR THRESHOLD SILL AREA. REMOVED CORROSION AS REQ AND FOUND OUT OF LIMITS IAW SRM 53-60-02. INSTALLED DOUBLER AND SPACER PER SRM 53-60-0
- [SDR DALA2017052304138](https://openairdocs.org/sdr/DALA2017052304138), May 20, 2017: SMOKE DETECTOR. FALSE ACTIVATION. LAVATORY SMOKE MESSAGE ON OAP. PERFORMED OPERATION CHECKS IAW MM. OPERATION CHECKS GOOD.
- [SDR DALA2016071805396](https://openairdocs.org/sdr/DALA2016071805396), Jul 15, 2016: WIRE. SHORTED. RIGHT EXTERNAL OVERWING EMERGENCY ESCAPE LIGHT INOPERATIVE. FOUND OPEN WIRE L1598B18N. REPAIRED THE WIRE, OPS CHECKED GOOD.
- [SDR DALA2015110606794](https://openairdocs.org/sdr/DALA2015110606794), Nov 4, 2015: GIRT BAR. OUT OF ADJUST. L1 DOOR GIRT BAR WOULD NOT ENGAGE FORWARD END. ADJUSTED LATCH SHIMS. OPS CHECKS OK.
- [SDR DALA2015103006752](https://openairdocs.org/sdr/DALA2015103006752), Oct 28, 2015: KEELBEAM. CRACKED. CRACK ON FORMER FORWARD SIDE, BS 1003 X=-6 TO X=6, KEEL BEAM. REPLACED IAW SRM 51-10-03, 51-10-05, 51-30-02, 51-30-05 AND DWG 5930584, REV BY.
- [SDR DALA2015111006858](https://openairdocs.org/sdr/DALA2015111006858), Oct 27, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520AT LT WING. FOUND OUT OF LIMITS. REPLACED FUEL PANEL.
- [SDR DALA2015102906750](https://openairdocs.org/sdr/DALA2015102906750), Oct 27, 2015: KEELBEAM. CRACKED. CRACK ON LT KEEL BEAM, NLG WHEEL WELL DOOR JAMB, BS 45 X=18. REPAIRED IAW SRM 53-90-01, FIG 6.
- [SDR DALA2015102706561](https://openairdocs.org/sdr/DALA2015102706561), Oct 26, 2015: ANGLE. CRACKED. CRACK ON LT & RT FORWARD ANGLES AT KEEL BEAM, BS 1007, X -6 AND X 6. REPLACED ANGLES IAW SRM 51-30-02 AND 51-30-05.
- [SDR DALA2015102606510](https://openairdocs.org/sdr/DALA2015102606510), Oct 25, 2015: SKIN. DAMAGED. LIGHTNING STRIKE ON LOWER FORWARD CORNER AND AFT EDGE WINDOW BETWEEN BETWEEN BS 693 AND 712, RT SIDE. REPAIRED IAW ETI-90-15-082, R1, REV AND ERA 539893-14, REV
- [SDR DALA2015102606509](https://openairdocs.org/sdr/DALA2015102606509), Oct 25, 2015: DOOR FRAME. CORRODED. CORROSION ON PREVIOUS REPAIR LOWER BEAM AT AFT CARGO COMPARTMENT DOOR JAMB. REPAIRED IAW ERA 539880-14, REV O AND SRM 53-60-02, FIG 9.
- [SDR DALA2015102606511](https://openairdocs.org/sdr/DALA2015102606511), Oct 24, 2015: TAB. DAMAGED. EXPOSED MATERIAL COMPOUND ON LT ELEVATOR CONTROL TAB. REPAIRED IAW SRM 55-21-01, PAR 4B.
- [SDR DALA2015111006857](https://openairdocs.org/sdr/DALA2015111006857), Oct 23, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520EB LT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCES PANEL.
- [SDR DALA2015102406508](https://openairdocs.org/sdr/DALA2015102406508), Oct 22, 2015: INTERCOSTAL. CRACKED. CRACKS ON INTERCOSTAL BETWEEN, BS 1542 AND 154 RT SIDE AT AFT ACC COMPARTMENT. R & R IAW DWG 9910087, REV 2 AND SRM 51-10-03, 51-30-02 AND 51-30-05.
- [SDR DALA2015102406507](https://openairdocs.org/sdr/DALA2015102406507), Oct 22, 2015: INTERCOSTAL. CRACKED. CRACK ON CANT INTERCOSTAL, BS 1555 RT SIDE AFT ACC COMPARTMENT. REPLACED IAW DWG 9910087, REV AD AND SRM 51-30-02, 51-30-05 AND 51-10-03.
- [SDR DALA2015102306505](https://openairdocs.org/sdr/DALA2015102306505), Oct 22, 2015: HOUSING. WORN. WEAR AT FORWARD CARGO DOOR HANDLE HOUSING. REPLACED IAW SRM 51-30-02 AND 51-30-05.
- [SDR DALA2015102206504](https://openairdocs.org/sdr/DALA2015102206504), Oct 21, 2015: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL BETWEEN BS 1364 - 1374, LONGERON 26 TO 27. REPLACED IAW SRM 51-30-02, 51-10-03, PARA 14 -21 AND DWG 5936667, REV BZ.
- [SDR DALA2015102206503](https://openairdocs.org/sdr/DALA2015102206503), Oct 20, 2015: FRAME. CORRODED. CORROSION ON FRAME ANGLE BS 1344 BETWEEN LONGERON 27 - 29R. REPAIRED IAW SRM 53-10-02.
- [SDR DALA2015102106502](https://openairdocs.org/sdr/DALA2015102106502), Oct 20, 2015: CUSP WEB. CRACKED. CRACK UNDER CUSP WEB AT BS 864 BELOW SEAT TRACK RBL 54. REPAIRED IAW SRM 51-30-02 AND 51-10-03, PARA 14 ADN 21.
- [SDR DALA2015110906832](https://openairdocs.org/sdr/DALA2015110906832), Oct 19, 2015: SKIN. CORRODED. CORROSION ON LT WING UPPER SKIN AT BS XRS 248, 295, 315, 353, AND 412. LOCATION XRS 315 IS OUT OF LIMITS. ROTO PEENING WAS APPLIED IAW SRM 57-30-01 AND 51-10-03
- [SDR DALA2015102106501](https://openairdocs.org/sdr/DALA2015102106501), Oct 19, 2015: WIRE. BROKEN. BROKEN WIRES ON LANYARD OF L1 DOOR. R & R LANYARD.
- [SDR DALA2015102106500](https://openairdocs.org/sdr/DALA2015102106500), Oct 19, 2015: RIB SPLICE. CRACKED. CRACKED SPLICE ON FIXED L/E, APPROXIMATELY XRS 164 LT WING. R & R THE RIBSPLICE, AND ANGLE IAW SRM 57-30-01, 51-10-03 AND 51-10-02.
- [SDR DALA2015102006499](https://openairdocs.org/sdr/DALA2015102006499), Oct 19, 2015: SKIN. CORRODED. CORROSION ON BARREL NUT HOLE NR 11 AT LT HORIZONTAL STABILIZER UPPER SURFACE, BS XH=7. REPAIRED IAW ETI-90-15-084, REV 1 AND ERA 539891-14, REV O.
- [SDR DALA2015101906348](https://openairdocs.org/sdr/DALA2015101906348), Oct 18, 2015: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB BETWEEN BS 218-237, X=-54 AND X=-60. R & R CUSP WEB AND RING DOUBLER IAW SRM 51-30-02, 53-20-02, FIG 18.
- [SDR DALA2015111006856](https://openairdocs.org/sdr/DALA2015111006856), Oct 17, 2015: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520 CT AND 620CT LT WING. FOUND OUT OF LIMITS. REPLACED PANEL.
- [SDR DALA2015101906350](https://openairdocs.org/sdr/DALA2015101906350), Oct 17, 2015: FRAME. CRACKED. CRACKED FRAME IN BS 180 BETWEEN LONGERON 5L-4L. REMOVED, FABRICATED AND INSTALLED NEW FRAME IAW SRM 51-30-02, 51-30-05 AND 51-10-03, PARA 14 AND 21.
- [SDR DALA2015101906349](https://openairdocs.org/sdr/DALA2015101906349), Oct 17, 2015: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORT AT BS 200 BETWEEN -7 TO 7. REPLACED FLOORBEAM IAW SRM 53-10-01 AND 51-10-03, 51-30-05 AND 51-30-02.
- [SDR DALA2015101906347](https://openairdocs.org/sdr/DALA2015101906347), Oct 17, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 160-200 BETWEEN X=54 AND 44 AND BS 148-200, X=7 TO-7. REPLACED IAW SRM 53-10-01, 51-10-03, 51-10-05, 51-30-05 AND 51-30-02.
- [SDR DALA2015111006855](https://openairdocs.org/sdr/DALA2015111006855), Oct 16, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520FT RT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.
- [SDR DALA2015111006854](https://openairdocs.org/sdr/DALA2015111006854), Oct 16, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 620FT. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.
- [SDR DALA2015101806340](https://openairdocs.org/sdr/DALA2015101806340), Oct 16, 2015: FITTING. CORRODED. CORROSION ON FORWARD/AFT FITTING BUSHING ON AFT CONEBOLT AT LEFT PYLON. NEW BUSHING INSTALLED IAW DWG 5965645, REV B.
- [SDR DALA2016102807901](https://openairdocs.org/sdr/DALA2016102807901), Oct 15, 2015: SKIN. CORRODED. CORROSION ON SKIN , BS 952 - 960 BETWEEN X -48 AND X -54. REPAIRED IAW ERA 539882-14, REV O.
- [SDR DALA2015111006853](https://openairdocs.org/sdr/DALA2015111006853), Oct 15, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINKS AND SETTLEMENT AREAS OF FUEL ACCESS PLANTE 620CB RT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.
- [SDR DALA2015111006852](https://openairdocs.org/sdr/DALA2015111006852), Oct 15, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 520CB LT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PANEL.
- [SDR DALA2015101706339](https://openairdocs.org/sdr/DALA2015101706339), Oct 15, 2015: DOUBLER. CORRODED. CORRODED PRODUCTION DOUBLER ON AFT PRESSURE BULKHEAD, BS 1395, LONGERON 29L-29R, AFT CARGO COMPARTMENT. REPLACED IAW DWG 5910130, REV ET AND SRM 51-30-02.
- [SDR DALA2015101606338](https://openairdocs.org/sdr/DALA2015101606338), Oct 15, 2015: SKIN. BENT. L1 DOOR EXTERNAL LOWER SKIN BENT. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND HINGE IAW SRM 51-10-03, PAR 14 AND 21, 52-10-01, FIG 4, 51-30-01 AND 51-3
- [SDR DALA2015101606346](https://openairdocs.org/sdr/DALA2015101606346), Oct 15, 2015: DOOR FRAME. CRACKED. CRACK ON DRILL HOLE HITTING AT R1 FORWARD LOWER DOOR JAMB. REPAIRED IAW ERA 539892-14, REV O AND ETI-90-15-085.
- [SDR DALA2015101406345](https://openairdocs.org/sdr/DALA2015101406345), Oct 13, 2015: STOP FITTING. CRACKED. CRACK ON FORWARD CARGO COMPARTMENT DOOR AFT EDGE STOPS NR 6 AND NR 8. REPLACED STOPPED FITTING NR 3 IAW SRM 51-30-01 AND 51-30-05.
- [SDR DALA2015101406343](https://openairdocs.org/sdr/DALA2015101406343), Oct 13, 2015: STIFFENER. CRACKED. CRACK ON STIFFENER AT P DOME, BS 1395. R & R STIFFENER IAW SRM 51-30-05 AND 51-30-02.
- [SDR DALA2015111006851](https://openairdocs.org/sdr/DALA2015111006851), Oct 12, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620DT RT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PLATE.
- [SDR DALA2015111006850](https://openairdocs.org/sdr/DALA2015111006850), Oct 12, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 620 RT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PLATE.
- [SDR DALA2015111006849](https://openairdocs.org/sdr/DALA2015111006849), Oct 12, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 520DT AT LT WING. FOUND OUT OF LIMITS. REPLACED PANEL ON AMDS 5730-0433.
- [SDR DALA2015101306342](https://openairdocs.org/sdr/DALA2015101306342), Oct 10, 2015: BEAM. CRACKED. L1 DOOR BEAM CRACKED FORWARD/AFT ENDS. REPAIRED IAW SRM 51-30-02, 51-30-01, 52-10-02, FIG 5 AND 51-30-02.
- [SDR DALA2015100806007](https://openairdocs.org/sdr/DALA2015100806007), Oct 8, 2015: WEB. CORRODED. CORROSION FOUND ON WEB, X-54 TO X-60 BETWEEN BS 617 - 636. REMOVED, FABRICATED AND REPLACED WEB IAW SRM 51-10-03.
- [SDR DALA2015101406344](https://openairdocs.org/sdr/DALA2015101406344), Oct 7, 2015: STOP FITTING. CRACKED. CRACK ON MID CARGO COMPARTMENT DOOR STOP, NR 2 AT AFT EDGE. REPLACED IAW SRM 51-30-01 AND 51-30-05.
- [SDR DALA1515069229](https://openairdocs.org/sdr/DALA1515069229), Jul 1, 2015: LONGERON. DAMAGED. LONGERON L2L AND L2R, SPLICE REPAIR, BS 1475, REPAIRED IAW ERA 537329-14MA.

All 107: https://openairdocs.org/aircraft/N929DN/reports.md

## STCs that may be installed (OpenAirDocs) (119, 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-90-30)

- [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 ST03815AT-D](https://openairdocs.org/stc/ST03815AT-D): Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST03966AT](https://openairdocs.org/stc/ST03966AT): Lavatory refurbishment and PED power installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04231AT](https://openairdocs.org/stc/ST04231AT): PED power installation. 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 ST01541AT-D](https://openairdocs.org/stc/ST01541AT-D): Installation of Collins DLM-900 ACARS Management unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [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 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 ST00275LA](https://openairdocs.org/stc/ST00275LA): Installation of Passenger Service Cart. Safran Cabin Inc
- [STC ST01056LA](https://openairdocs.org/stc/ST01056LA): Installation of galleys, closet, stowage SIA, forward lavatory, bin, class divider (movable), sidewall and ceiling panels. Safran Cabin Inc
- [STC ST01336LA](https://openairdocs.org/stc/ST01336LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01990LA-D](https://openairdocs.org/stc/ST01990LA-D): Installation of Overhead Stowage Bin Extension Kits. Safran Cabin Inc
- [STC ST01991LA-D](https://openairdocs.org/stc/ST01991LA-D): Interior Installations. Safran Cabin Inc
- [STC ST01998LA-D](https://openairdocs.org/stc/ST01998LA-D): Installation of Overhead Stowage Bin Kits. Safran Cabin Inc
- [STC ST02255LA](https://openairdocs.org/stc/ST02255LA): Modification and installation of Window Shades. Safran Cabin 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 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 ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST01932AT](https://openairdocs.org/stc/ST01932AT): Installation of SAF-T-GLO Aerospace Limited's photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [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 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 ST03988AT](https://openairdocs.org/stc/ST03988AT): Installation of the EMTEQ LED Lights in the main cabin. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [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 ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST00491SE](https://openairdocs.org/stc/ST00491SE): Installation of the AlliedSignal Enhanced Ground Proximity Warning System. Honeywell International Inc
- [STC ST01023SE](https://openairdocs.org/stc/ST01023SE): Installation of a the TPA-81A Traffic Alert and Collision Avoidance System (TCAS) Processor in accordance with Master Drawing List 756-0119-001, Revision D, dated November 21, 2003, or later FAA approved revisions. Honeywell International Inc
- [STC ST01915AT](https://openairdocs.org/stc/ST01915AT): Installation of a RDR-4B Weather Radar/Windshear System. Honeywell International Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST02541CH](https://openairdocs.org/stc/ST02541CH): Installation of an Aircell Broadband Services (ABS) System. Intelsat Inflight LLC
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST02502LA](https://openairdocs.org/stc/ST02502LA): Installation of TDG Aerospace, Inc. Universal Fault Interrupter (UFI). TDG Aerospace Inc
- [STC ST04167CH](https://openairdocs.org/stc/ST04167CH): Installation of CMC CMA-5024 GLSSU units and ACSS NXT-800 Mode S Transponders. Canard Aerospace Corporation
- [STC ST04283AT](https://openairdocs.org/stc/ST04283AT): Interior Modification to add a Cart Stowage unit. Delta Air Lines Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA8339SW](https://openairdocs.org/stc/SA8339SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC ST01395AT-D](https://openairdocs.org/stc/ST01395AT-D): Installation of Collins DLM-700 B ACARS system installed with a Miltope Printer. HAECO Cabin Solutions LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC

All 119: https://openairdocs.org/aircraft/N929DN/stcs.md

## Related

- Other Mcdonnell Douglas MD-90-30 aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-90-30/aircraft.md
- The IAE V2500SERIES engine: https://openairdocs.org/engine/iae-v2500series.md

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