McDonnell Douglas DC-9: Difference between revisions

DC-9
A New York Air DC-9-32, 1983
Role	Narrow-body jet airliner
Manufacturer	Douglas Aircraft McDonnell Douglas
First flight	February 25, 1965
Introduction	December 8, 1965 with Delta Air Lines
Status	In service
Primary users	Delta Air Lines USA Jet Airlines Everts Air Cargo
Produced	1965–1982
Number built	976
Variants	McDonnell Douglas MD-80 McDonnell Douglas MD-90 Boeing 717

The McDonnell Douglas DC-9 (initially known as the Douglas DC-9) is a twin-engine, single-aisle jet airliner. It was first manufactured in 1965 with its maiden flight later that year. The DC-9 was designed for frequent, short flights. The final DC-9 was delivered in October 1982.

The DC-9-based airliners, MD-80, MD-90 and Boeing 717 later followed in production. With the final two deliveries of the 717 in 2006, production of the DC-9/MD-80/90/717 aircraft family ceased after 41 years and over 2,400 units built.

Design and development

Origins

During the 1950s Douglas Aircraft studied a short-medium range airliner to complement their higher capacity, long range DC-8. (DC stands for Douglas Commercial.) A medium range four-engine Model 2067 was studied but it did not receive enough interest from airlines and it was abandoned. In 1960 Douglas signed a two-year contract with Sud Aviation for technical cooperation. Douglas would market and support the Sud Aviation Caravelle and produce a licensed version if airlines ordered large numbers, but none were ordered and Douglas returned to its design studies after the cooperation deal expired.

Northwest Airlines (NWA) DC-9 T-tail at Regina International Airport

In 1962 design studies were underway. The first version seated 63 passengers and had a gross weight of 69,000 lb (31,300 kg). This design was changed into what would be initial DC-9 variant. Douglas gave approval to produce the DC-9 on April 8, 1963. Unlike the competing but larger Boeing 727 trijet, which used as many 707 components as possible, the DC-9 was an all-new design. The DC-9 has two rear-mounted Pratt & Whitney JT8D turbofan engines, relatively small, efficient wings, and a T-tail. The DC-9's takeoff weight was limited to 80,000 lb (36,300 kg) for a two-person flight crew by Federal Aviation Agency regulations at the time. DC-9 aircraft have five seats across for economy seating. The airplane seats 80 to 135 passengers depending on version and seating arrangement.

The DC-9 was designed for short to medium routes, often to smaller airports with shorter runways and less ground infrastructure than the major airports being served by larger designs like the Boeing 707 and Douglas DC-8. Accessibility and short field characteristics were called for. The tail mounted engine design facilitated a clean wing without engine pods, which had numerous advantages. For example, flaps could be longer, unimpeded by pods on the leading edge and engine blast concerns on the trailing edge. This simplified design improved airflow at low speeds and enabled lower takeoff and approach speeds, thus lowering field length requirements and keeping wing structure light.

The second advantage of the tail-mounted engines was the reduction in foreign object damage from ingested debris from runways and aprons. Third, the absence of engines in underslung pods allowed a reduction in ground clearance, making the aircraft more accessible to baggage handlers and passengers. Turnarounds were simplified by built-in airstairs, including one in the tail, which shortened boarding and deplaning times. The problem of deep stalling, revealed by the loss of the BAC One-Eleven prototype in 1963, was overcome through various changes, including the introduction of vortilons, small surfaces beneath the wing's leading edge used to control airflow and increase low speed lift.

Into production

C-9 Nightingale used for Aeromedical Evacuation

The first DC-9, a production model, flew on February 25, 1965. The second DC-9 flew a few weeks later, with a test fleet of five aircraft flying by July. This allowed the initial Series 10 to gain airworthiness certification on November 23, 1965, and to enter service with Delta Air Lines on December 8. The DC-9 was always intended to be available in multiple versions to suit customer requirements, The first stretched version, the Series 30, with a longer fuselage and extended wing tips, flew on August 1, 1966, entering service with Eastern Air Lines in 1967. The initial Series 10 would be followed by the improved -20, -30, and -40 variants. The final DC-9 series was the -50, which first flew in 1974.

In 1967, the US Air Force selected the DC-9 to meet their requirement for a medical evacuation (MedEvac) and passenger transport aircraft, designated as the C-9A Nightingale; deliveries began in 1968. The U.S. Navy also ordered five C-9Bs for passenger and cargo duties in April 1972. The C-9B aircraft have provided air logistics support for the Navy and Marine Corps. A C-9B was also chosen by NASA for reduced gravity research. Some C-9s were converted from former civilian DC-9s; three were also specially configured for VIP transport duties. Kuwait also operated a small C-9 fleet. All USAF C-9s were retired by 2005.

A Cebu Pacific DC-9 in 2006

The DC-9 was a commercial success with 976 built when production ended in 1982. The DC-9 is one of the longest-lasting aircraft in operation. Its reliability and efficiency led to sales of its successors into the 21st century. The DC-9 family is one of the most successful jet airliners with a total of over 2,400 units produced; it ranks third behind the second-place Airbus A320 family with over 5,000 produced, and the first-place Boeing 737 with over 7,000 produced.

Studies aimed at further improving DC-9 fuel efficiency, by means of retrofitted wingtips of various types, were undertaken by McDonnell Douglas. However, these did not demonstrate significant benefits, especially with existing fleets shrinking. The wing design makes retrofitting difficult.

Legacy

The DC-9 was followed by the introduction of the MD-80 series in 1980. The MD-80 series was originally called DC-9-80 series. It was a lengthened DC-9-50 with a higher maximum takeoff weight (MTOW), a larger wing, new main landing gear, and higher fuel capacity. The MD-80 series features a number of variants of the Pratt & Whitney JT8D turbofan engine having higher thrust ratings than those available on the DC-9.

The MD-80 series was further developed into the McDonnell Douglas MD-90 in the early 1990s. It has yet another fuselage stretch, a glass cockpit (first introduced on the MD-88) and completely new International Aero V2500 high-bypass turbofan engines. In comparison to the very successful MD-80, relatively few MD-90s were built.

The final variant was the MD-95, which was renamed the Boeing 717-200 after McDonnell Douglas's merger with Boeing in 1997 and before aircraft deliveries began. The fuselage length and wing are very similar to the DC-9-30, but much use was made of lighter, modern materials. Power is supplied by two BMW/Rolls-Royce BR715 high bypass turbofan engines.

China's Comac ARJ21 is derived from the DC-9 family. The ARJ21 is built with manufacturing tooling from the MD-90 Trunkliner program. Consequently it has the same fuselage cross section, nose profile and tail.

Variants

British Midland Airways DC-9-15

Series 10

The original DC-9 (later designated the Series 10) was the smallest DC-9 variant. The -10 was 104.4 ft (31.8 m) long and had a maximum weight of 82,000 lb (37,000 kg). The Series 10 was similar in size and configuration to the BAC One-Eleven and featured a T-tail and rear mounted engines. Power was provided by a pair of 12,500 lbf (56 kN) Pratt & Whitney JT8D-5 or 14,000 lbf (62 kN) JT8D-7 engines. A total of 137 were built. Delta Air Lines was the initial operator.

The Series 10 was produced in two main subvariants, the Series 14 and 15, although of the first four aircraft, three were built as Series 11s and one as Series 12. These were later converted to Series 14 standard. No Series 13 was produced. A passenger/cargo version of the aircraft with a 136 x 81 in side cargo door forward of the wing and a reinforced cabin floor, was certificated on March 1, 1967. Cargo versions included the Series 15MC (Minimum Change) with folding seats which can be carried at the rear of the aircraft, and the Series 15RC (Rapid Change) with seats removable on pallets. These differences disappeared over the years as new interiors have been installed.

The Series 10 was unique in the DC-9 family in not having leading edge slats. The Series 10 was designed to have short takeoff and landing distances without the use of leading edge high-lift devices. Therefore, the wing design of the Series 10 featured airfoils with extremely high maximum lift capability in order to obtain the low stalling speeds necessary for short field performance.

Series 10 features

The Series 10 has an overall length of 104.4 feet (31.82 m), a fuselage length of 92.1 feet (28.07 m), a passenger cabin length of 60 feet (18.29 m), and a wingspan of 89.4 feet (27.25 m).

The Series 10 was offered with the 14,000 lbf (62 kN) thrust JT8D-1 and JT8D-7.

All versions of the DC-9 are equipped with an AlliedSignal (Garrett) GTCP85 APU, located in the aft fuselage.

The Series 14 was originally certificated at an MTOW of 85,700 lb (38,900 kg) but subsequent options offered increases to 86,300 and 90,700 lb (41,100 kg). The aircraft's MLW in all cases is 81,700 lb (37,100 kg). The Series 14 has a fuel capacity of 3,693 US gallons (with the 907 US gal centre section fuel). The Series 15, certificated on January 21, 1966, is physically identical to the Series 14 but has the increased MTOW of 90,700 lb (41,100 kg). Typical range with 50 passengers and baggage is 950 nmi (1,760 km), increasing to 1,278 nmi (2,367 km) at long range cruise. Range with maximum payload is 600 nmi (1,100 km), increasing to 1,450 nmi (2,690 km) with full fuel.

The DC-9 Series 10, as with all later versions of the DC-9 is equipped with a two crew analog flightdeck.

The aircraft is fitted with a passenger door in the port forward fuselage, and a service door/emergency exit is installed opposite. An airstair installed below the front passenger door was available as an option as was an airstair in the tailcone. This also doubled as an emergency exit. Available with either two or four overwing exits, the DC-9-10 can seat up to a maximum certified exit limit of 109 passengers. Typical all economy layout is 90 passengers, and 72 passengers in a more typical mixed-class layout with 12 first and 60 economy-class passengers.

All versions of the DC-9 are equipped with a tricycle undercarriage, featuring a twin nose unit and twin main units.

Series 20

Scandinavian Airlines DC-9-21

The Series 20 was designed to satisfy a Scandinavian Airlines request for improved short field performance by using the more powerful engines and improved wings of the -30 combined with the shorter fuselage used in the -10. Ten Series 20 aircraft were produced, all of them Model -21.

In 1969, a DC-9 Series 20 at Long Beach was fitted with an Elliott Flight Automation Head-up display by McDonnell Douglas and used for successful three month-long trials with pilots from various airlines, the Federal Aviation Administration, and the US Air Force.

Series 20 features

The Series 20 has an overall length of 104.4 feet (31.82 m), a fuselage length of 92.1 feet (28.07 m), a passenger cabin length of 60 feet (18.29 m), and a wingspan of 93.3 feet (28.44 m).

The DC-9 Series 20 is powered by the 15,000 lbf (67 kN) thrust JT8D-11 engine.

The Series 20 was originally certificated at an MTOW of 94,500 lb (42,900 kg) but this was increased to 98,000 lb (44,000 kg), some 8 percent up on the higher weight Series 14s and 15s. The aircraft's MLW is 95,300 lb (43,200 kg) and MZFW is 84,000 lb (38,000 kg). Typical range with maximum payload is 1,000 nmi (1,900 km), increasing to 1,450 nmi (2,690 km) with maximum fuel. The Series 20, using the same wing as the Series 30, 40 and 50, has a slightly lower basic fuel capacity than the Series 10 (3,679 US gallons).

Series 20 milestones

• First flight: September 18, 1968.
• FAA certification: November 25, 1968.
• First delivery: December 11, 1968 to SAS
• Entry into service: January 27, 1969 with SAS.
• Last delivery: May 1, 1969 to SAS.

Series 30

Ex-Spirit Airlines DC-9-30 Firebird II, highly modified as a surveillance aircraft for the U.S. Navy, based at Mojave Airport

The -30 was produced to counter Boeing's 737 twinjet; 662 were built, about 60% of the total. The -30 entered service with Eastern Airlines in February 1967 with a 14 ft 9 in (4.50 m) fuselage stretch, wingspan increased by just over 3 ft (0.9 m) and full-span leading edge slats, improving takeoff and landing performance. Maximum takeoff weight was typically 110,000 lb (50,000 kg). Engines for Models -31, -32, -33 and -34 included the P&W JT8D-7 and JT8D-9 rated at 14,500 lbf (64 kN) of thrust, or JT8D-11 with 15,000 lbf (67 kN).

Unlike the -10, the Series 30 had leading edge devices to reduce the landing speeds at higher landing weights; full-span slats reduced approach speeds by 6 knots despite 5000 lbs greater weight. The slats were lighter than slotted Krueger flaps, since the structure associated with the slat is a more efficient torque box than the structure associated with the slotted Krueger. The wing had a six percent increase in chord, all ahead of the front spar, allowing the 15 percent chord slat to be incorporated.

Series 30 variants

TAA DC-9-30 at Melbourne Airport, 1987

The Series 30 was built in four main sub-variants.

• DC-9-31: Produced in passenger version only. The first DC-9 Series 30 flew on August 1, 1966, and the first delivery was to Eastern Airlines on February 27, 1967 after certification on December 19, 1966. Basic MTOW of 98,000 lb (44,000 kg) and subsequently certificated at weights up to 108,000 lb (49,000 kg).
• DC-9-32: Introduced in the first year (1967). Certificated March 1, 1967. Basic MTOW of 108,000 lb (49,000 kg) later increased to 110,000 lb (50,000 kg). A number of cargo versions of the Series 32 were also produced:
  • 32LWF (Light Weight Freight) with modified cabin but no cargo door or reinforced floor, intended for package freighter use.
  • 32CF (Convertible Freighter), with a reinforced floor but retaining passenger facilities
  • 32AF (All Freight), a windowless all-cargo aircraft.
• DC-9-33: Following the Series 31 and 32 came the Series 33 for passenger/cargo or all-cargo use. Certificated on April 15, 1968, the aircraft's MTOW was 114,000 lb (52,000 kg), MLW to 102,000 lb (46,000 kg) and MZFW to 95,500 lb (43,300 kg). JT8D-9 or -11 (15,000 lbf (67 kN) thrust) engines were used. Wing incidence was increased 1.25 degrees to reduce cruise drag. Only 22 were built, as All Freight (AF), Convertible Freight (CF) and Rapid Change (RC) aircraft.
• DC-9-34: The last variant was the Series 34, intended for longer range with an MTOW of 121,000 lb (55,000 kg), an MLW of 110,000 lb (50,000 kg) and an MZFW of 98,000 lb (44,000 kg). The DC-9-34CF (Convertible Freighter) was certificated April 20, 1976, while the passenger followed on November 3, 1976. The aircraft has the more powerful JT8D-9s with the -15 and -17 engines as an option. It had the wing incidence change introduced on the DC-9-33. Twelve were built, five as convertible freighters.

Series 30 features

The DC-9-30 was offered with a selection of variants of JT8D including the -1, -7, -9, -11, -15 and -17. The most common on the Series 31 is the JT8D-7 (14,000 lbf (62 kN) thrust), although it was also available with the -9 and -17 engines. On the Series 32 the JT8D-9 (14,500 lbf (64 kN) thrust) was standard, with the -11 also offered. The Series 33 was offered with the JT8D-9 or -11 (15,000 lbf (67 kN) thrust) engines and the heavyweight -34 with the JT8D-9, -15 (15,000 lbf (67 kN) thrust) or -17 (16,000 lbf (71 kN) thrust) engines.

Series 40

DC-9-40 flight deck

This further lengthened version entered service with SAS in March 1968. With a 6 ft 6 in (2 m) longer fuselage, accommodation was up to 125 passengers. The -40 was fitted with Pratt & Whitney engines of between 14,500 and 16,000 lbf (64 and 71 kN). A total of 71 were produced.

Series 50

The -50 was the largest DC-9 to fly. It features an 8 ft 2 in (2.49 m) fuselage stretch and seats up to 139 passengers. It started revenue service in August 1975 with Eastern Airlines and included a number of detail improvements, a new cabin interior, and more powerful JT8D-15 or -17 engines in the 16,000 and 16,500 lbf (71 and 73 kN) class. McDonnell Douglas delivered 96, all as Model -51. Some visual cues to distinguish this version from other DC-9 variants include side strakes (fins) below the side cockpit windows and thrust reversers rotated about 22 degrees on the original configuration. However various maintenance replacements have seen the thrust reversers in the same position as the -30 and -40.

For later DC-9 variants, see McDonnell Douglas MD-80, McDonnell Douglas MD-90, and Boeing 717.

Delta DC-9-51 Interior Cabin View N779NC

Military and government

A US Air Force C-9A Nightingale

• C-9A Nightingale - 23 aeromedical evacuation aircraft for the United States Air Force received from 1968. The final active-duty flight of the C-9A was in September 2005. The last C-9A was flown to Andrews AFB Museum in September 2012.
• C-9B Skytrain II - 24 convertible passenger/transport versions for the United States Navy and Marine Corps delivered from 1973 to 1976. An additional five C-9s were converted from passenger configured DC-9s.
• VC-9C - 3 executive transport aircraft for the United States Air Force. The three aircraft were delivered to the US Air Force in late 1976.
• C-9K - 2 DC-9-30C for the Kuwait Air Force.

Operators

Two British Midland DC-9s at Teesside Airport in 1994.

Perris Valley Skydiving DC-9-21, January 2008

A total of 129 DC-9 aircraft (all variants) were in commercial service as of November 2011, including Delta Air Lines (21), USA Jet Airlines (7), Everts Air Cargo (5), Aeronaves TSM (4), Aserca Airlines (4), LASER Airlines (4), Aeropostal (2) and other operators with fewer aircraft.

Delta Air Lines has, since acquiring Northwest Airlines, operated a fleet of DC-9 aircraft, most of which are over 30 years old. With severe increases in fuel prices in the summer of 2008, Northwest Airlines finally began retiring its DC-9s, switching to Airbus A319s that are 27% more fuel efficient.

Because of the usage of the aging JT8D engines, as of late 2000s (decade) DC-9s are considered gas guzzlers when compared to other more recent airliner designs. Studies aimed at improving DC-9 fuel efficiency, by means of retrofitted wingtip extensions of various types, have not succeeded in demonstrating significant benefits.

With the existing DC-9 fleet shrinking, modifications do not appear to be likely to occur, especially since the wing design makes retrofitting difficult. Thus, DC-9s are likely to be further replaced in service by new Boeing 737, Airbus A320, Embraer E-Jets aircraft, or the new, emerging Bombardier CSeries airliner. However, it is probable that a modest number of DC-9s will continue to productively fly for many years to come. As the Northwest/Delta merger progressed, Delta pulled several stored DC-9s back into service.

One ex-SAS DC-9-21 is operated as a skydiving jump platform at Perris Valley Airport in Perris, California. With the steps on the ventral stairs removed, it is the only airline transport class jet certified to date by the FAA for skydiving operations as of 2008.

Deliveries

Deliveries

Type	Total	1982	1981	1980	1979	1978	1977	1976	1975	1974	1973	1972	1971	1970	1969	1968	1967	1966	1965
DC-9-10	113															10	29	69	5
DC-9-10C	24															4	20
DC-9-20	10														9	1
DC-9-30	585	8	10	13	24		1	12	16	21	21	17	42	41	97	161	101
DC-9-30C	30					1		6				4	1	3	5	7	3
DC-9-30F	6														4	2
DC-9-40	71				5	6	3	2	4	27		3	2	7	2	10
DC-9-50	96		5	5	10	15	18	28	15
C-9A	21											8	1		5	7
C-9B	17	2	1					2	4		8
VC-9C	3								3
Total	976	10	16	18	39	22	22	50	42	48	29	32	46	51	122	202	153	69	5

Accidents and incidents

As of March 2009, the DC-9 has been involved in 117 incidents, including 101 hull-loss accidents, with 2,135 fatalities.

Notable accidents

• On October 1, 1966, West Coast Airlines Flight 956 crashed with eighteen fatalities and no survivors. This accident marks the first loss of a DC-9.
• On March 9, 1967, TWA Flight 553 fell to earth in a field in Concord Township, near Urbana, Ohio, following a mid-air collision with a Beechcraft Baron, an accident which triggered substantial changes in air traffic control procedures. All 25 people on board the DC-9 were killed.
• On March 17, 1969, Viasa Flight 742 crashed into the La Trinidad neighborhood of Maracaibo during a failed take-off. All 84 people on board the aircraft as well as 71 people on the ground were killed. At that time Viasa Flight 742 was the worst disaster in aviation history.
• On June 27, 1969, Douglas DC-9-31 N906H of Hawaiian Airlines collided on the ground with Vickers Viscount N7410 of Aloha Airlines at Honolulu International Airport. The Viscount was damaged beyond repair.
• On September 9, 1969, Allegheny Airlines Flight 853, a DC-9-30, collided in mid-air with a Piper PA-28 Cherokee near Fairland, Indiana. The DC-9 carried 78 passengers and 4 crew members, the Piper one pilot. The occupants of both aircraft were killed in the accident and the aircraft were destroyed.
• On February 15, 1970, a Dominicana de Aviación DC-9 crashed after taking off from Santo Domingo, in what is known as the Dominicana DC-9 air disaster. The crash, possibly caused by contaminated fuel, killed all 102 passengers and crew, including champion boxer Teo Cruz.
• On May 2, 1970, an Overseas National Airways DC-9, wet-leased to ALM Dutch Antilles Airlines and operating as ALM Flight 980, ditched in the Caribbean Sea on a flight from New York's John F. Kennedy International Airport to Princess Juliana International Airport on Sint Maarten. After three landing attempts in poor weather at Sint Maarten, the pilots began to divert to their alternate of Saint Croix, U.S. Virgin Islands but ran out of fuel 30 mi (48 km) short of the island. After about 10 minutes, the aircraft sank in 5,000 ft (1524 m) of water and was never recovered. 40 people survived the ditching, 23 perished.
• On November 14, 1970, Southern Airways Flight 932, a DC-9, crashed into a hill near Tri-State Airport in Huntington, West Virginia. All 75 on board were killed (including 37 members of the Marshall University Thundering Herd football team, eight members of the coaching staff, 25 boosters, and others).
• On January 26, 1972, Jugoslovenski Aero Transport Flight 367, in flight from Copenhagen to Belgrade, DC-9-32 registration YU-AHT, was destroyed in flight by a bomb placed on board. The sole survivor was a flight attendant, Vesna Vulović, who holds the record for the world's longest fall without a parachute when she fell some 33,000 ft (10,000 m) inside the tail section of the airplane and survived.
• On November 10-11, 1972, Southern Airways Flight 49 was hijacked while departing Birmingham, Alabama's airport by three armed men. The hijackers then proceeded to fly the passengers and crew to multiple locations in the United States, Canada, and Cuba, including Chattanooga, Tennessee, where the less-than-demanded ransom money was delivered, the now-defunct McCoy Air Force Base in Orlando, Florida, where the FBI shot out two of the DC-9's four main landing wheels, and Havana, where the 30 hours and 4,000 miles (6,400 km) odyssey came to an end with no fatalities or injuries between the passengers and crew members. This incident is notable for being the first hijacking in which an aircraft left Cuba with the hijackers onboard.
• On December 20, 1972, North Central Airlines Flight 575, DC-9-31 registration N954N, collided during its takeoff roll with Delta Air Lines Flight 954, a Convair CV-880 that was taxiing across the same runway at O'Hare International Airport in Chicago, Illinois, in what is known as the 1972 Chicago-O'Hare runway collision. The DC-9 was destroyed, killing 10 and injuring 15 of the 45 people on board; two people among the 93 aboard the Convair 880 suffered minor injuries.
• On July 31, 1973, Delta Air Lines Flight 723, DC-9-31 registration N975NE, crashed into a seawall at Logan International Airport in Boston, Massachusetts, killing all 83 passengers and 6 crew members on board. One of the passengers initially survived the accident but later died in a hospital.
• On September 11, 1974, Eastern Air Lines Flight 212, a DC-9-30 crashed just short of the runway at Charlotte, North Carolina, killing 71 out of the 82 occupants.
• On 30 October 1975, an Inex-Adria Aviopromet DC-9-32 hit high ground during an approach in fog near Prague-Suchdol, Czechoslovakia. 75 people were killed.
• On September 10, 1976, an Inex-Adria Aviopromet DC-9 collided with a British Airways Trident over the Croatian town of Vrbovec, killing all 176 people aboard both aircraft, in what is known as the 1976 Zagreb mid-air collision.
• On April 4, 1977, Southern Airways Flight 242, a DC-9-31, lost engine power in a storm then crash landed onto a highway in New Hope, Georgia, US, striking road side buildings. The crash and fire resulted in the death of both flight crew and 61 passengers. Nine people on the ground also died. Both flight attendants and 20 passengers survived.
• On June 26, 1978, Air Canada Flight 189, a DC-9 overran the runway in Toronto after a blown tire aborted the takeoff. Two of the 107 passengers and crew were killed.
• On September 14, 1979, Aero Trasporti Italiani Flight 12, a DC-9-32 crashed in the mountains near Cagliari, Italy while approaching Cagliari-Elmas Airport. All 27 passengers and 4 crew members died in the crash and ensuing fire.

An Itavia DC-9 (registration I-TIGI) which was lost in an accident at Ustica in 1980.

• On June 27, 1980, Aerolinee Itavia Flight 870, a DC-9-15 suffered an in-flight explosion and crashed into the sea near the Italian island of Ustica. All 81 people on board were killed. The causes of this accident are still unclear.

Itavia DC-9 (I-TIGI) was destroyed in an accident at Ustica. Shown in the "Museo della Memoria" opened in Bologna in 2007.

• On July 27, 1981, Aeromexico Flight 230 ran off the runway in Chihuahua. Bad weather and pilot error were blamed.
• On June 2, 1983, Air Canada Flight 797, a DC-9 experienced an electrical fire in the aft lavatory during flight, resulting in an emergency landing at Cincinnati/Northern Kentucky International Airport. During evacuation, the sudden influx of oxygen caused a flash fire throughout the cabin, resulting in the deaths of 23 of the 41 passengers, including Canadian folk singer Stan Rogers. All five crew members survived.
• On December 7, 1983, the Madrid Runway Disaster took place where a departing Iberia Boeing 727 struck an Aviaco Douglas DC-9 causing the death of 93 passengers and crew. All 42 passengers and crew on board the DC-9 were killed.
• On August 31, 1986, Aeroméxico Flight 498 collided in mid-air with a Piper Cherokee over the city of Cerritos, California, then crashed into the city, killing all 67 aboard the aircraft, 15 people on the ground, and all 3 in the small plane.
• On 4 April 1987, Garuda Indonesia Flight 035, a DC-9-32, hit a pylon and crashed on approach to Polonia International Airport in bad weather with 24 fatalities.
• On December 3, 1990, Northwest Airlines Flight 1482, a DC-9-14, went on the wrong taxiway in dense fog at Detroit-Metropolitan Wayne County Airport, Michigan (DTW). It entered the active runway instead of taxiway instructed by air traffic controllers. It collided with a departing Northwest Boeing 727. Nine people were killed.
• On July 2, 1994, USAir Flight 1016 crashed in Charlotte, North Carolina while performing a go-around because of heavy storms and wind shear at the approach of runway 18R. There were 37 fatalities and 15 injured among the passengers and crew. Although the airplane came to rest in a residential area with the tail section striking a house, there were no fatalities or injuries on the ground.
• On May 11, 1996 ValuJet Flight 592 crashed in the Florida Everglades due to a fire caused by the activation of chemical oxygen generators illegally stored in the hold. The fire damaged the plane's electrical system and eventually overcame the crew, resulting in the deaths of 110 people.
• On October 10, 1997 (1997-10-10), Austral Flight 2553, DC-9-32 registration LV-WEG, en route from Posadas to Buenos Aires, crashed near Fray Bentos, Uruguay, killing 74 people (69 passengers and 5 crew).
• On February 2, 1998, Cebu Pacific Flight 387 crashed on the slopes of Mount Sumagaya in Misamis Oriental, Philippines, killing all 104 people on board. Aviation investigators deemed the incident to be caused by pilot error when the plane made a non-regular stopover to Tacloban.
• On November 9, 1999, TAESA Flight 725 crashed a few minutes after leaving the Uruapan Airport en route to Mexico City. 18 people were killed in the accident.
• On October 6, 2000, Aeroméxico Flight 250, a DC-9-31 en route from Mexico City to Reynosa, Mexico, could not stop at end of runway and crashed into houses and fell into a small canal. Four people on the ground were killed. None of 83 passengers and 5 crew members were killed. The DC-9 was heavily damaged and classified as a loss. The runway had seen heavy rainfall as a result of Hurricane Keith.
• On April 15, 2008, a Hewa Bora Airways DC-9 crashed into a residential neighborhood, in the Goma, Democratic Republic of the Congo, resulting in the deaths of at least 44 people, in what is known as the 2008 Goma DC-9 crash.
• On July 6, 2008, USA Jet Airlines Flight 199, a DC-9-15F, after taking off from Shreveport, LA airport bound for Saltillo, Mexico crashed and burned. The captain was killed and first officer was seriously injured. The cause of the crash is under investigation.

Aircraft on display

• XA-TBX ex-Aerocaribe- Preserved at Venustiano Carranza at Benito Juarez International Airport as a public hi-tech library
• ex-N8903E Northwest Airlines- Preserved at TVF since 15-04-1998 as a donation to the Northland Community & Technical College
• ex-Air Canada C16Y70 preserved and on display at the Canada Aviation Museum
• ex-Iberia Airways EC-BQZ-CY105 Preserved at MAD on display between terminals 1 and 2, used as theater by AENA

Specifications

	DC-9-15	DC-9-20	DC-9-30	DC-9-40	DC-9-50
Flight crew	2
Passengers (1 class)	90		115	125	135
Length	104 ft 4¾ in (31.82 m)		119 ft 3½ in (36.37 m)	125 ft 7¼ in (38.28 m)	133 ft 7¼ in (40.72 m)
Wingspan	89 ft 5 in (27.25 m)	93 ft 5 in (28.47 m)
Height	27 ft 6 in (8.38 m)			28 ft 0 in (8.53 m)
Wing Area	934.3 sq ft (86.77 m²)	1,000.7 sq ft (92.97 m²)
Aspect ratio	8.55:1	8.71:1
Empty weight	49020 lb (22,235 kg)	52,880 lb (23,880 kg)	57,190 lb (25,940 kg)	58,670 lb (26,612 kg)	61,880 lb (28,068 kg)
Max takeoff weight	90,700 lb (41,100 kg)	98,000 lb (44,500 kg)	108,000 lb (49,090 kg)	114,000 lb (51,700 kg)	121,000 lb (54,900 kg)
Powerplants (2x)	P&W JT8D-5 or -7	P&W JT8D-11	P&W JT8D-7, -9, -11, -15 or -17	P&W JT8D-9, -11, -15 or -17	P&W JT8D-15 or -17
Engine thrust	12,250 to 14,000 lbf (54.5 to 62.3 kN)	14,500 lbf (64.5 kN)	14,000 to 16,000 lbf (62.3 to 71.2 kN)	14,500 to 16,000 lbf (64.5 to 71.2 kN)	15,500 to 16,000 lbf (69 to 71.2 kN)
Max cruise (at 25,000 ft (7,620 m))	490 kn (564 mph, 907 km/h)	494 kn (569 mph, 915 km/h)	490 kn (565 mph, 907 km/h)	485 kn (558 mph, 898 km/h)
Max range	1,590 nmi (1,831 mi, 2,946 km)	1,605 nmi (1,848 mi, 2,974 km)	1,670 nmi (1,923 mi, 3,095 km)	1,555 nmi (1,790 mi, 2,880 km)	1,795 nmi (2,067 mi, 3,326 km)
Fuel capacity	3,700 US gallons (14,000 L)	3,679 US gallons (13,930 L)			5,038 US gallons (19,070 L)

Allegheny Airlines DC-9-30 c. 1970

Comparison of McDonnell Douglas DC-9, Boeing 717, and different McDonnell Douglas MD-80 derivatives

• Cabin cross section:
  • External width: 10 ft 11.6 in (3.34 m)
  • Internal width: 10 ft 3.7 in (3.14 m)
  • External height: 11 ft 8 in (3.6 m)
  • Internal height: 6 ft 9 in (2.06 m)

Source: Jane's All The World's Aircraft 1976–77 except where specified.

See also

• Airstair
• N900SA

Related development

• McDonnell Douglas MD-80
• McDonnell Douglas MD-90
• Boeing 717
• COMAC ARJ21

Aircraft of comparable role, configuration, and era

• BAC One-Eleven
• Boeing 737
• Fokker F28
• Sud Aviation Caravelle
• Tupolev Tu-134

Related lists

• List of civil aircraft

References

Bibliography

• Becher, Thomas. Douglas Twinjets, DC-9, MD-80, MD-90 and Boeing 717. The Crowood Press, 2002. ISBN 1-86126-446-1.
• "Super 80 For the Eighties". Air International, Vol 18 No 6, June 1980. pp. 267–272, 292–296. ISSN 0306-5634.
• Taylor, John W. R. Jane's All The World's Aircraft 1966–67. London: Sampson Low, Marston & Company, 1966.
• Taylor, John W. R. Jane's All The World's Aircraft 1976–77. London: Jane's Yearbooks, 1976. ISBN 0-354-00538-3.

External links

• DC-9 page on Boeing.com
• DC-9 history page on Boeing.com
• DC-9-10/20/30 on Airliners.net and DC-9-40/50 on Airliners.net
• DC-9 History on AviationHistoryOnline.com