# Boeing MD-90-30

- Type: Aircraft model (FAA registry)
- Registry code: 13848ME
- Manufacturer (registry): BOEING
- Model: MD-90-30
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 142
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 2
- Page: https://openairdocs.org/model/boeing-md-90-30

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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

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/model/boeing-md-90-30/ads.md

## Information bulletins (advisory) (4)

- [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

## Registered aircraft (2)

- [N931TB](https://openairdocs.org/aircraft/N931TB): [Boeing Company](https://openairdocs.org/faa-owner/BOEING%20COMPANY), [Renton, WA](https://openairdocs.org/faa-place/WA/Renton), built 1998, S/N 53532
- [N963DN](https://openairdocs.org/aircraft/N963DN): [Boeing Company](https://openairdocs.org/faa-owner/BOEING%20COMPANY), [Renton, WA](https://openairdocs.org/faa-place/WA/Renton), built 1999, S/N 53533

## NTSB investigations

None matched to aircraft with this model.

## 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 20130624012709I](https://openairdocs.org/incident/20130624012709I), Jun 24, 2013: Boeing MD-90-30 (N963DN), Washington, DC, Minor damage. Delta airlines flight 1763, an MD-90, N963DN, departing Ronald Reagan Washington national airport (kdca) to minneapolis-st. paul international airport (kmsp),…

## Service difficulty reports (6,066, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR DALA2020080602719](https://openairdocs.org/sdr/DALA2020080602719), Aug 5, 2020: ATTACH ANGLE. CRACKED. CRACK ON RH ATTACH ANGLE THROUGH ACCESS PANEL 370AL. NRC 00156: RH ATTACH ANGLE WAS REPLACED IAW DWG #5912188 REV BD AND MD-90 SRM 51-30-02 AND 51-30-05 VOL.II.
- [SDR DALA2020080542718](https://openairdocs.org/sdr/DALA2020080542718), Aug 4, 2020: FRAME. CRACKED. CRACK ON FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT (CAT). NRC 00251: FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER MD-90 
- [SDR DALA2020030601662](https://openairdocs.org/sdr/DALA2020030601662), Mar 5, 2020: BATTERY PACK. DISCHARGED. FOUND LWR EMERGENCY PATH LIGHTS ON BOTH FWD DOORS INOP. R/R EMERGENCY LIGHT SLID AND BATTERY PACK B5-211 PER MD90 AM;33 -51. OPS CHECK GOOD . A/C OK FOR SVC. (6
- [SDR DALA2020030301548](https://openairdocs.org/sdr/DALA2020030301548), Feb 25, 2020: FASTENER. MISSING. LOOSE AND MISSING FASTENERS ABOVE SPLICE STA ZFS= 52.267 AT VERTICAL STABILIZER LEADING EDGE (EHV) SUMMARY NRC 00491: VERTICAL STABILIZER LEADING EDGE WAS REPAI
- [SDR DALA2020022601419](https://openairdocs.org/sdr/DALA2020022601419), Feb 25, 2020: BEAM. CRACKED. INITIAL INSPECTION: CRACKED RH DOOR JAMB BEAM ON STA 45 AND X=- 18 AT NLG WHEEL WELL AREA (FYT) ENTR 00983062 W SUMMARY OF NRC 600:RH DOOR JAMB BEAM ON STA 45 A
- [SDR DALA2020022501377](https://openairdocs.org/sdr/DALA2020022501377), Feb 24, 2020: FAN. FAILED. LEFT HEAT EXCHANGER COOLING FAN POPS ALL 3 PHSES C/B'S. ODOR THROUGHOUT CABIN C/A R/R LT HEAT EXCHANGER COOLING FAN PER MD90AMM 21-55. LEAK AND FUNCTIONAL CKS G
- [SDR DALA2020022431349](https://openairdocs.org/sdr/DALA2020022431349), Feb 22, 2020: SKIN. CRACKED. INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA Y=1437 BTW LONG 13-13RH (FUS) SUMMARY OF NRC S/N 00161: FUSELAGE SKIN STA Y=1437 BTW LONG 13- 13RH WAS REPAIRED P
- [SDR DALA2020022421348](https://openairdocs.org/sdr/DALA2020022421348), Feb 21, 2020: SKIN. DAMAGED. INITIAL INSPECTION: WORN AND BENTED PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN ON L1 DOOR HOLD OPEN ATTACH POINT (FUS) SUMMARY OF NRC 00100. PREVIOUS REPAIR DOUBL
- [SDR DALA2020022421347](https://openairdocs.org/sdr/DALA2020022421347), Feb 21, 2020: TORQUE TUBE. CRACKED. CRACKED VENTRAL STAIR WAY TORQUE TUBE BEAM AT AFT ACCESSORY COMPARTMENT (CAT) LOG-PAGE UPDATED SUMMARY OF NRC 00794. VENTRAL STAIR WAY TORQUE TUBE BEAM AT AFT A
- [SDR DALA2020022421346](https://openairdocs.org/sdr/DALA2020022421346), Feb 21, 2020: FLOOR SUPPORT. CORRODED. CORROSION ON L2 LOWER SILL INTERCOSTAL BTW STA 720/740 AND 63 LBL PASSENGER CABIN (W2) LOG-PAGE UPDATED SUMMARY OF NRC 00359 CORROSION LEVEL 2 LOWER SILL BTW ST
- [SDR DALA2020022101310](https://openairdocs.org/sdr/DALA2020022101310), Feb 20, 2020: DOOR FRAME. CORRODED. CORROSION ON DOOR JAMB WEB STA 1212-1220 BTW PROJECTION LONGS 29RH-28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 SUMMARY OF NRC 00334: CORROSION LEVEL 2: WEB OF S
- [SDR DALA2020022101309](https://openairdocs.org/sdr/DALA2020022101309), Feb 20, 2020: SKIN. CORRODED. CORROSION ON FUSELAJE SKIN STA=864 AND STR- 28R TO STR- 29R. SUMMARY OF NRC 00198: CORROSION (LEVEL 2) ON FUSELAJE SKIN STA= 864 AND STR- 28R TO STR- 29R WAS RE
- [SDR DALA2020021901242](https://openairdocs.org/sdr/DALA2020021901242), Feb 19, 2020: COFFEEMAKER. FAILED. DURING CLIMB, FLT ATTEND'S SMELLED ODOR FROM COFFEE MKR. COFFEE MAKER WAS EXTREMELY HOT, SMELLED LIKE ELECTRICAL BURN NEAR CKPT DOOR. I TURNED OFF GALLEY PWR. A
- [SDR DALA2020021901238](https://openairdocs.org/sdr/DALA2020021901238), Feb 19, 2020: DOOR FRAME. CRACKED. INITIAL INSPECTION: CRACKED LH DOOR JAMB BEAM ON STA 48 AND X=18 AT NLG WHEEL WELL AREA (FYT) LOG-PAGE UPDATED SUMMARY OF NRC 00601: LH DOOR JAMB BEAM ON STA 48
- [SDR DALA2020021901246](https://openairdocs.org/sdr/DALA2020021901246), Feb 18, 2020: LONGERON. CRACKED. INITIAL INSPECTION: CRACKED LONGERON 2RH ON STA 1475 AT AFT ACCESSORY COMPARTMENT (CAT) SUMMARY OF NRC S/N 00785: LONGERON WAS REPAIRED PER ER/A 564080- 14MA RE
- [SDR DALA2020021901241](https://openairdocs.org/sdr/DALA2020021901241), Feb 18, 2020: SKIN. CORRODED. AWR HIDDEN CORROSION IN REF NRC 895. DURING REMOTION OF VAPOR BARRIER WAS FOUND CORROSION ON CENTER WING UPPER SKIN STA 943- 962 BTW X=-44 TO X=-60 AT WING BOX 
- [SDR DALA2020021901240](https://openairdocs.org/sdr/DALA2020021901240), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 992 BTW X=44 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF NRC 00891. CORROSION LEVEL 1. CORROSIO
- [SDR DALA2020021901239](https://openairdocs.org/sdr/DALA2020021901239), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY. OF NRC 0888. CORROSION LE
- [SDR DALA2020021801200](https://openairdocs.org/sdr/DALA2020021801200), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00884, CORROSION
- [SDR DALA2020021801199](https://openairdocs.org/sdr/DALA2020021801199), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00885, CORROSION
- [SDR DALA2020021801198](https://openairdocs.org/sdr/DALA2020021801198), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ; OF NRC 889, CORROSION LE
- [SDR DALA2020021801197](https://openairdocs.org/sdr/DALA2020021801197), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 943 TO 962 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ;OF NRC 00890, CORROSION L
- [SDR DALA2020021801196](https://openairdocs.org/sdr/DALA2020021801196), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 883 TO 902 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00887: CORROSIO
- [SDR DALA2020021801195](https://openairdocs.org/sdr/DALA2020021801195), Feb 18, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 962 TO 984 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00886: CORROS
- [SDR DALA2020021801194](https://openairdocs.org/sdr/DALA2020021801194), Feb 18, 2020: INTERCOSTAL. CORRODED. INITIAL INSPECTION: CORROSION ON INTERCOSTAL STA 1205-1210 BTW LONGS 30 AND 29RH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00349: CORROSION LE
- [SDR DALA2020021801193](https://openairdocs.org/sdr/DALA2020021801193), Feb 18, 2020: FRAME ANGLE. CORRODED. INITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1379 BTW LONGS 29RH TO 26RH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00552: FRAME CLIP STA 13
- [SDR DALA2020021761187](https://openairdocs.org/sdr/DALA2020021761187), Feb 16, 2020: FRAME ANGLE. CORRODED. INITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1364 BTW LONGS 28RH TO 27LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00303. CORROSION LEVEL 2
- [SDR DALA2020021761186](https://openairdocs.org/sdr/DALA2020021761186), Feb 16, 2020: FRAME ANGLE. CORRODED. INITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1269 BTW LONGS 29RH TO 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00328: CORROSION LEVEL 2
- [SDR DALA2020021761185](https://openairdocs.org/sdr/DALA2020021761185), Feb 16, 2020: LONGERON. CORRODED. INITIAL INSPECTION: CORROSION ON LONGERON END 27RH STA 1395 AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) LOG-PAGE UPDATED RII: N ENTR 00897853 W SUMMARY OF NRC 
- [SDR DALA2020021761184](https://openairdocs.org/sdr/DALA2020021761184), Feb 16, 2020: LONGERON. CORRODED. INITIAL INSPECTION: CORROSION ON LONGERON END 28RH STA 1395 AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00557. CORROSION LEVEL 2 LONGERON END 28
- [SDR DALA2020021761183](https://openairdocs.org/sdr/DALA2020021761183), Feb 15, 2020: SKIN. CRACKED. INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA Y=1494 BTW LONG 2 -3 LH (FUS) LOG-PAGE UPDATED SUMMARY OF NRC 00591: SKIN STA Y=1494 BTW LONG 2-3 LH WAS REPAIRED
- [SDR DALA2020021761182](https://openairdocs.org/sdr/DALA2020021761182), Feb 15, 2020: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00555. CORR
- [SDR DALA2020021761181](https://openairdocs.org/sdr/DALA2020021761181), Feb 15, 2020: STRUCTURE. CORRODED. INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00555. CORR
- [SDR DALA2020021761180](https://openairdocs.org/sdr/DALA2020021761180), Feb 15, 2020: DOOR FRAME. CORRODED. INITIAL INSPECTION: CORROSION ON DOOR JAMB WEB STA 360-370 BTW LONGS 28RH AND 26RH AT FWD CARGO COMPARTMENT MRB 53-302-07 (CCD) SUMMARY ; OF NRC 00827 ; LEVEL C
- [SDR DALA2020021761179](https://openairdocs.org/sdr/DALA2020021761179), Feb 15, 2020: SEAT TRACK. CORRODED. INITIAL INSPECTION: CORROSION ON LH SEAT TRACK X=54 STA 745-750, 765-770, 775-780, 795,800, 805-810 AND 825-840 MRB 53-211-02 ( CPAX) SUMMARY ; OF NRC 103 ; NEW
- [SDR DALA2020021761178](https://openairdocs.org/sdr/DALA2020021761178), Feb 15, 2020: SEAT TRACK. CORRODED. INITIAL INSPECTION: CORROSION ON LH SEAT TRACK X=54 STA 620-625, 640-650, 670-675, 690-695, 700-705, 710-715 AND 730-735 MRB 53- 211-02 (CPAX) SUMMARY ; OF NRC 
- [SDR DALA2020021401139](https://openairdocs.org/sdr/DALA2020021401139), Feb 14, 2020: PAN. CRACKED. INITIAL INSPECTION: CRACK ON LH AFT EMERGENCY EXIT DOOR JAMB PAN UPPER AREA (FUS) SUMMARY OF NRC 00162. LH AFT EMERGENCY EXIT DOOR JAMB PAN UPPER AREA (FUS) WAS
- [SDR DALA2020021401140](https://openairdocs.org/sdr/DALA2020021401140), Feb 13, 2020: DOOR FRAME. CORRODED. CORROSION ON MID CARGO COMPT LOWER DOOR JAMB STA 695 TO 750 MRB 53-122-02 (CCC) SUMMARY OF NR 00206. LEVEL CORROSION II. MID CARGO COMPT LOWER DOOR JAMB STA 695
- [SDR DALA2020021401138](https://openairdocs.org/sdr/DALA2020021401138), Feb 13, 2020: FRAME. CRACKED. CRACK ON CAP STA Y= 1364 LONG 7LH AT PASSENGER CABIN (CPAX) SUMMARY OF NRC S/N 01063: CAP STA Y= 1364 LONG 7LH AT PASSENGER CABIN WAS REPAIRED PER ER/A 585192-1
- [SDR DALA2020021401137](https://openairdocs.org/sdr/DALA2020021401137), Feb 13, 2020: FRAME. CORRODED. CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT). SUMMARY OF NRC 00554. CORROSION LEVEL 2 PREVI
- [SDR DALA2020021301108](https://openairdocs.org/sdr/DALA2020021301108), Feb 12, 2020: HYDRAULIC SYSTEM. LEAKING. UPON LANDING RIGHT HYDRAULIC QUANTITY RAPIDLY DROPPED TO 4 QTS. F/A NOTIFIED US DURING TAXI A SMELL OF HYDRAULIC FLUID BURNING C/A VERIFIED LEAK FROM TAIL DRAIN
- [SDR DALA2020021301107](https://openairdocs.org/sdr/DALA2020021301107), Feb 12, 2020: CHANNEL. CORRODED. CORROSION ON PREVIOUS REPAIR CHANNEL AND STRAP FRAME STA 1344 BTW LONGS 28RH TO 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) NRC 00301. CORROSION LEVEL 2 P
- [SDR DALA2020021101075](https://openairdocs.org/sdr/DALA2020021101075), Feb 11, 2020: FITTING. CORRODED. CORROSION ON FWD AND AFT FITTING AT AFT CARGO COMPT LOWER DOOR JAMB STA 1211 AND 1268 (CCT) MRB 53-123- 02 NRC 00202. CORROSION LEVEL 2. FITTING AT AFT CARGO CO
- [SDR DALA2020021101074](https://openairdocs.org/sdr/DALA2020021101074), Feb 10, 2020: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB BTW STA 718-736 BTW X=-44 AND X=-60 MRB 53?211?01 (CPAX) SUMMARY OF NRC 01239: (LEVEL CORROSION 2), SECTION RH CUSP WEB OUT LIMIT BTW S
- [SDR DALA2020021101073](https://openairdocs.org/sdr/DALA2020021101073), Feb 10, 2020: FRAME. CORRODED. CORROSION ON PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) NRC 00550. CORROSION LEVEL 2. PREVIOUS REPAIR 
- [SDR DALA2020021101072](https://openairdocs.org/sdr/DALA2020021101072), Feb 10, 2020: SKIN. DAMAGED. RE-WRITE FROM NRC 0415: INITIAL INSPECTION: BEND EXTERNAL LOWER PREVIOUS REPAIR AT FWD ENTRANCE DOOR (L1) (PTAS)". REASON FOR RE-WRITE: PREVIOUS REPAIR CANT BE 
- [SDR DALA2020021101071](https://openairdocs.org/sdr/DALA2020021101071), Feb 10, 2020: FRAME. CORRODED. CORROSION ON PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00549. CORROSION LEVEL 2.PREVIO
- [SDR DALA2020021101070](https://openairdocs.org/sdr/DALA2020021101070), Feb 10, 2020: FRAME ANGLE. CORRODED. CORROSION ON FRAME CLIP AT AFT CARGO COMPARTMENT STA 1344 AND BETWEEN L27-R AND L26-R. (C3) CORROSION LEVEL 2: FRAME CLIP AT AFT CARGO COMPARTMENT STA 1344 AND 
- [SDR DALA2020021101069](https://openairdocs.org/sdr/DALA2020021101069), Feb 10, 2020: WINDOW FRAME. CRACKED. CRACK ON FRAME OF CLEAR VIEW WINDOW LH, UPPER AFT CORNER. (CPIL) INTERNAL DOUBLER WAS REPLACED PER MD90 SRM VOL II 51-30-02 AND 51-30-05 AND DWG 5911356 REV. DJ
- [SDR DALA2020021001037](https://openairdocs.org/sdr/DALA2020021001037), Feb 9, 2020: WINDOW FRAME. CRACKED. AWR HIDDEN CRACK: IN REF NRC 01010 AFTER DOUBLER WAS REMOVED HIDDEN CRACK WAS FOUND ON UPPER AFT SKIN CORNER OF RH CLEARVIEW WINDOW (CPIL) SUMMARY NRC 01243:UPP

All 6,066: https://openairdocs.org/model/boeing-md-90-30/reports.md

## STCs that may be installed (OpenAirDocs) (119, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [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/model/boeing-md-90-30/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Mcdonnell Douglas MD-90-30](https://openairdocs.org/model/mcdonnell-douglas-md-90-30): 3 registered aircraft, registry code 3023690
- [Mcdonnell Douglas MD-90-30](https://openairdocs.org/model/mcdonnell-douglas-md-90-30): 0 registered aircraft, registry code 302369A

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