# N8079U: Mcdonnell Douglas DC-8-71F, registration cancelled 2001-09-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 6, 2001
- Status when cancelled: Triennial form not returned
- Airframe: [Mcdonnell Douglas DC-8-71F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-71f) (registry code 302199G)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 45947
- Type of aircraft: Fixed wing multi engine
- Certificate issued: April 21, 1998
- Last registry action: April 17, 2001
- Mode S code: AAFF84
- Owner when cancelled: [Emery Worldwide Airlines Inc](https://openairdocs.org/faa-owner/EMERY%20WORLDWIDE%20AIRLINES%20INC)
- Location: [Redwood City, CA](https://openairdocs.org/faa-place/CA/Redwood%20City)
- Owner type: Corporation
- Owner's area on the map: 37.5334° N, 122.2496° W: Placed by OpenAirDocs at the center of ZIP code 94065, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8079U
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8079U
- Page: https://openairdocs.org/deregistered/N8079U-2001-09-06

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-8-71F: https://openairdocs.org/model/mcdonnell-douglas-dc-8-71f.md

## Service difficulty reports (84, newest 50)

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

- [SDR 99T64R545EWA](https://openairdocs.org/sdr/99T64R545EWA), Nov 19, 1999: PIN BOSS. CORRODED. DURING D-CHECK. LT MAIN GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO 99-174 WITH A
- [SDR 99T64R533EWA](https://openairdocs.org/sdr/99T64R533EWA), Nov 13, 1999: FASTENER. MISSING. FOUND DURING D-CHECK. RT WING L/E ABOVE NR PYLON. ONE LOOSE FASTENER WITH SKIN WASHER, ONE FASTENER MISSING. (EO). TIGHTENED THE LOOSE FASTENER. INSTALLED NAS16
- [SDR 2000T74R547EW](https://openairdocs.org/sdr/2000T74R547EW), Nov 12, 1999: METAL STRIP. CRACKED. DURING C-CHECK. NR 2 ENGINE LT SIDE METAL STRIP ABOVE REVERSER COWL HAS .75 INCH CRACK. NDT TO DETERMINE LENGTH OF CRACK. STOP DRILLED AND NDT TO CONFIRM CRACK.
- [SDR 99T64R535EWA](https://openairdocs.org/sdr/99T64R535EWA), Nov 11, 1999: FASTENER. MISSING. FOUND DURING D-CHECK. RT MAIN LANDING GEAR FITTING MISSING FASTENER AFT SIDE. (EO). LEFT THE SHEARED SHANK IN THE HOLE, FILLED HOLE WITH PR1422B 1/2 SEAL. IT IS
- [SDR 99T64R539EWA](https://openairdocs.org/sdr/99T64R539EWA), Nov 10, 1999: DOOR. MISSING. DURING D-CHECK. FABRICATED AND INSTALLED DIVIDER WALL BETWEEN C AND D PITS. (EO). FABRICATED A NEW DOOR USING DRAWING 99-174-2. TREATED AND PRIMED PER EO 999-17
- [SDR 99T64R534EWA](https://openairdocs.org/sdr/99T64R534EWA), Nov 9, 1999: PIN BOSS. CORRODED. FOUND DURING D-CHECK. RT MAIN LANDING GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO
- [SDR 99T64R504EWA](https://openairdocs.org/sdr/99T64R504EWA), Nov 8, 1999: DRAIN PLUG. MISSING. FOUND DURING D-CHECK. C-PIT DOOR MISSING DRAIN PLUG. FABRICATED FILLER. TREATED AND PRIMED. INSTALLED FILLERS AND DRAIN PLUG PER EO 99-174 WITH APPROVED 8110-3 
- [SDR 99T64R444EWA](https://openairdocs.org/sdr/99T64R444EWA), Nov 4, 1999: BULKHEAD. DAMAGED. FOUND DURING D-CHECK. 'A' PIT AFT BULKHEAD BOTTOM NEEDS TO BE TRIMMED STA 440. (EO). FABRICATED NEW DOOR USING DRAWING NR 99-174-1. TREATED AND PRIMED IAW EO 99
- [SDR RRXA991790](https://openairdocs.org/sdr/RRXA991790), Nov 3, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 660 TO STA 750. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED A
- [SDR RRXA991789](https://openairdocs.org/sdr/RRXA991789), Nov 3, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 750 TO STA 860. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED A
- [SDR RRXA991788](https://openairdocs.org/sdr/RRXA991788), Nov 3, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 40 TO STA 80 AND BETWEEN BL 56L TO BL 68L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM
- [SDR RRXA991787](https://openairdocs.org/sdr/RRXA991787), Nov 3, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 1240 TO STA 1348 AND BETWEEN BL 48L TO BL 62L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8
- [SDR RRXA991786](https://openairdocs.org/sdr/RRXA991786), Nov 3, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 340 TO STA 346. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED A
- [SDR 99T64R537EWA](https://openairdocs.org/sdr/99T64R537EWA), Nov 3, 1999: PANEL. BROKEN. FOUND DURING D-CHECK. STA 1660 SIDE RAIL PANEL BROKEN STA 1650 - STA 1700. (EO). FABRICATED NEW SIDE RAIL PANEL PER EO 99-174 WITH APPROVED 8110-3 DATED 10-20-9
- [SDR RRXA991779](https://openairdocs.org/sdr/RRXA991779), Nov 2, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA=-69 BETWEEN BL=0 TO BL=45L AND WL-9.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAG
- [SDR 99T64R532EWA](https://openairdocs.org/sdr/99T64R532EWA), Oct 27, 1999: VANE. DAMAGED. FOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 5 VANE INBOARD UPPER END HAS ELONGATED HOLE. DRILLED AND REAMED HOLE TO .75 INCH DIAMETER. TREATED AND PRIMED. FABR
- [SDR 99T64R518EWA](https://openairdocs.org/sdr/99T64R518EWA), Oct 27, 1999: SKIN. DAMAGED. FOUND DURING D-CHECK. LEFT WING OUTBOARD FLAP VANE INBOARD END UPPER SURFACE HAS IMPROPER REPAIR OF ELONGATED HOLE. DRILLED AND REAMED HOLE TO .375 INCH DIAMETE
- [SDR 99T64R452EWA](https://openairdocs.org/sdr/99T64R452EWA), Oct 26, 1999: ACTUATOR CRANK. CRACKED. FOUND DURING D-CHECK. RIGHT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRACK ON FLAP ACTUATOR ASSEMBLY IAW DC-8 OHM 27-28-7
- [SDR 99T64R451EWA](https://openairdocs.org/sdr/99T64R451EWA), Oct 26, 1999: ACTUATOR CRANK. CRACKED. FOUND DURING D-CHECK. LT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRANK ON FLAP ACTUATOR ASSY IAW DC-8 OHM 27-28-7. REF: 
- [SDR 99T64R503EWA](https://openairdocs.org/sdr/99T64R503EWA), Oct 25, 1999: SKIN. DAMAGED. FOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 6 VANE INBOARD END TOP SIDE HAS HOLE ELONGATED. DRILLED AND REAMED HOLE TO .375 INCH. FABRICATED PLUG AND INSTALLED
- [SDR RRXA991780](https://openairdocs.org/sdr/RRXA991780), Oct 22, 1999: INTERCOSTAL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 980 TO STA 995 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMO
- [SDR 99T64R536EWA](https://openairdocs.org/sdr/99T64R536EWA), Oct 22, 1999: SKIN. DAMAGED. RIGHT INBOARD LEADING EDGE TOP MOUNT HOLES DAMAGED OR ELONGATED, 7 EACH. DRILLED, PRIMED AND INSTALLED IAW EO NR 99-174 WITH APPROVED 8110-3 DATED 9-14-99. REF:
- [SDR 99T64R538EWA](https://openairdocs.org/sdr/99T64R538EWA), Oct 18, 1999: KICK PLATE. CRACKED. FOUND DURING D-CHECK. AFT LOWER CARGO RACKS AND DENTS. (EO). STRAIGHTEN DENTS. NDT VERIFIED NO CRACKS, STOP DRILLED CRACKS AND WELDED IAW EO 99-174 WITH APPROVE
- [SDR 99T64R513EWA](https://openairdocs.org/sdr/99T64R513EWA), Oct 18, 1999: THRUST REVERSER. DAMAGED. FOUND DURING D-CHECK. RT FAN REV DAMAGED ON LOWER VERTICAL SURFACE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYST MIXED WITH MI
- [SDR 99T64R512EWA](https://openairdocs.org/sdr/99T64R512EWA), Oct 18, 1999: COWL. DAMAGED. FOUND DURING D-CHECK. HOLE ON INSIDE OF LT FORWARD OF LT FORWARD COWL NR 1 ENGINE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYS
- [SDR 99T64R508W](https://openairdocs.org/sdr/99T64R508W), Oct 18, 1999: KICK PLATE. DAMAGED. FOUND DURING D-CHECK. TYPE ONE EMERGENCY EXIT DOOR LEFT SIDE. KICK PLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAD BEEN STOPPED. WELDED KICK P
- [SDR 99T64R434EWA](https://openairdocs.org/sdr/99T64R434EWA), Oct 18, 1999: STIFFENER. BROKEN. LEFT WHEELWELL FORWARD WEBBING FRAME BROKEN. (EO). WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS FOUND. ACCEPTABLE TO RETURN TO SERVICE PER E
- [SDR 99T64R432EWA](https://openairdocs.org/sdr/99T64R432EWA), Oct 18, 1999: STIFFENER. BROKEN. RIGHT WHEELWELL FORWARD WEBBING STIFFENER BROKEN. (EO). WELDED NEW SECTION OF TUBING IAW MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-174 WITH APPROVED 81
- [SDR 99T64R514EWA](https://openairdocs.org/sdr/99T64R514EWA), Oct 15, 1999: LINE. CHAFED. FOUND DURING D-CHECK. FIRE RETARDANT LINE CHAFED FORWARD OF TOMBSTONE NR 3 PYLON. BLENDED CHAFE SMOOTH FILLED CHAFE WITH WELD, NDT WELD NO FLAWS FOUND PER EO 99
- [SDR 99T64R510EWA](https://openairdocs.org/sdr/99T64R510EWA), Oct 14, 1999: KICK PLATE. DAMAGED. FOUND DURING C-CHECK. TYPE ONE EMERGENCY DOOR RIGHT FORWARD KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAVE BEEN STOPPED, WELDED KICKPLAT
- [SDR 99T64R509EWA](https://openairdocs.org/sdr/99T64R509EWA), Oct 14, 1999: KICK PLATE. DAMAGED. FOUND DURING D-CHECK. TYPE ONE EMERGENCY DOOR AFT RIGHT SIDE KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAD BEEN STOPPED. WELDED KICKPLAT
- [SDR 99T64R507EWA](https://openairdocs.org/sdr/99T64R507EWA), Oct 12, 1999: KICK PLATE. GOUGED. FOUND DURING D-CHECK. B-PIT DOOR KICK PLATE GOUGED/SCRATCHED. (EO). FABRICATED NEW KICK PLATE. WELDED ACCORDING TO MIL-STD-2219, NDT WELD TO ASSURE NO FLAWS IN 
- [SDR 99T64R454EWA](https://openairdocs.org/sdr/99T64R454EWA), Oct 12, 1999: SKIN. DAMAGED. FOUND DURING D-CHECK. RT MID LEADING EDGE TWO DOUBLER LOWER EXTERIOR TO EVALUATE DAMAGE STA XFS 416.500 - XS 435.289. (EO). REMOVED AND REPLACED THE OUTBOARD EX
- [SDR RRXA991785](https://openairdocs.org/sdr/RRXA991785), Oct 8, 1999: INTERCOSTAL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 520 TO STA 540 AND LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM
- [SDR 99T64R515EWA](https://openairdocs.org/sdr/99T64R515EWA), Oct 8, 1999: THRUST REVERSER. LIGHTNING STRIKE. FOUND DURING D-CHECK. THREE LIGHTNING STRIKES, RIGHT FAN REV. TRAILING EDGE OUTER SECTION MIDDLE AND BOTTOM NR 4 ENGINE. (EO). BLENDED THE EDGE OF THE LIGHTNING
- [SDR 99T64R453EWA](https://openairdocs.org/sdr/99T64R453EWA), Oct 8, 1999: SKIN. DAMAGED. FOUND DURING D-CHECK, LT MID-WIND LEADING EDGE OUTBOARD END SLOT VANE STA 520.168, HOLES WORN AND ELONGATED. (EO). FABRICATED REPAIR STRAP 12 INCHES BY 2.25 INC
- [SDR 99T64R445EWA](https://openairdocs.org/sdr/99T64R445EWA), Oct 7, 1999: BUSHING MOUNT. CRACKED. FOUND DURING D-CHECK. AFT PASSENGER DOOR (L2) HAS CRACK AT UPPER HINGE BUSHING AREA STA 1600. REMOVED CRACK SECTION BY CUT OUT. FABRICATED REPAIR DOUBLERS. TREA
- [SDR 99664R428EWA](https://openairdocs.org/sdr/99664R428EWA), Oct 7, 1999: SKIN. DAMAGED. EXTERIOR RT LIGHTING STRIKE STA 250 RT BETWEEN L21R - L22R. (EO). BLENDED ROUGH AREAS SMOOTH, REAMED HOLES AND INSTALLED MS20470AD8 RIVET. TREATED AND PRIMED PE
- [SDR RRXA991781](https://openairdocs.org/sdr/RRXA991781), Oct 6, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1280 AND LONGERON 35 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED A
- [SDR 99T64R500EWA](https://openairdocs.org/sdr/99T64R500EWA), Oct 6, 1999: COVER. GOUGED. FOUND DURING D-CHECK. 'D' PIT DOOR THRESHOLD PLATE GOUGED/SCRATCHED STA 1420. (EO). REMOVED THE EXISTING D-PIT THRESHOLD PLATE. FABRICATED NEW THRESHOLD, WELDED
- [SDR 99T64R506EWA](https://openairdocs.org/sdr/99T64R506EWA), Oct 5, 1999: FRAME. CORRODED. FOUDN DURING D-CHECK. CORROSION AT STA -67 APPROXIMATELY 45 INCHES LEFT OF CENTER ON SUB-FLOOR FRAME IN COCKPIT. (EO). REMOVED CORROSION. TREATED, PRIMED AND FI
- [SDR 99T64R455EWA](https://openairdocs.org/sdr/99T64R455EWA), Oct 4, 1999: SKIN. LIGHTNING STRIKE. FOUND DURING D-CHECK. LIGHTNING STRIKE STA 300 RT BETWEEN L18R - L19R (EO). OPENED LIGHTNING STRIKE HOLE TO .375 INCH. FABRICATED DOUBLER AND INSTALLED PER EO 9
- [SDR RRXA991783](https://openairdocs.org/sdr/RRXA991783), Oct 3, 1999: BOLT. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CARGO DOOR T-BOLT BETWEEN STA 280 TO STA 340 AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR
- [SDR 99T64R440EWA](https://openairdocs.org/sdr/99T64R440EWA), Oct 2, 1999: RIB. CRACKED. LEFT WING T/E STA 261 FLAP WELL RIB CRACKED BELOW NR 4 SPOILER. CUT OUT CRACK. TREATED AND PRIMED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-174 WITH
- [SDR RRXA991784](https://openairdocs.org/sdr/RRXA991784), Oct 1, 1999: FRAME. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1420 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA I
- [SDR 99T64R426EWA](https://openairdocs.org/sdr/99T64R426EWA), Oct 1, 1999: SEAT TRACKS. WORN. F/E SEAT AFT TRACK LOCK HOLES WORN TO LIMITS. REMOVED AND REPLACED F/E'S SEAT TRACK IAW DC-8 SRM 51-1-21. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR 99T64R475EWA](https://openairdocs.org/sdr/99T64R475EWA), Sep 28, 1999: SKIN. DAMAGED. FOUND DURING D-CHECK, MID-WING LEADING EDGE SLOT VANE HOLE OVERSIZED AND WORN AT STA XS 520.186. (EO). CLEANED EXISTNG COUNTERSINKS, ALODINED, TREATED AND PRIME
- [SDR 99T64R429EWA](https://openairdocs.org/sdr/99T64R429EWA), Sep 25, 1999: SHIM. BROKEN. NR 3 STUB WING L/E INBOARD LOWER SPAR CAP SHIM BROKEN OFF XILD .7095. (EO). SMOOTHED REMAINING EDGE OF SHIM. NDT TO ASSURE THAT NO CRACKS EXIST. (NONE FOUND). T
- [SDR RRXA991782](https://openairdocs.org/sdr/RRXA991782), Sep 24, 1999: FINGER  DOUBLER. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA -25 AND BL 36L AND WL -9. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, T
- [SDR 99T64R467WEA](https://openairdocs.org/sdr/99T64R467WEA), Sep 23, 1999: RIB. CRACKED. FOUND DURING D-CHECK. NR 2 STUB WING LEADING EDGE, 7 INCH CRACK TOP RIB STA 250.089. STOP DRILLED CRACK IAW DC-8 SRM 57-2-0. FABRICATED TWO DOUBLERS IAW DC-8 SR

All 84: https://openairdocs.org/deregistered/N8079U-2001-09-06/reports.md

## NTSB investigations (2)

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

- [NTSB DCA00MA026](https://openairdocs.org/ntsb/DCA00MA026), Feb 17, 2000: Douglas DC-8-71F (N8079U), Rancho Cordova, CA, destroyed, 3 fatal. Probable cause: A loss of pitch control resulting from the disconnection of the right elevator control tab. The disconnection was caused by the failure to properly secure and inspect the attachment bolt.
- [NTSB MIA92IA077](https://openairdocs.org/ntsb/MIA92IA077), Feb 9, 1992: Douglas DC-8-71 (N8079U), Miami, FL, incident, minor damage. Probable cause: THE FAILURE OF THE FAA LOCAL CONTROLLER TO ASURE ADEQUATE CLEARANCE WAS ESTABLISHED.

## FAA accident and incident reports (5)

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.

- [Accident 20000216041589A](https://openairdocs.org/incident/20000216041589A), Feb 16, 2000: Doug DC871F (N8079U), Rancho Cordova, CA, Destroyed, 3 fatal. (-23) Aircraft departed mather field about 1949 pacific standard time (PST). Shortly after takeoff the crew declared and emergency to air traffic control and…
- [Incident 19970528022749I](https://openairdocs.org/incident/19970528022749I), May 28, 1997: Doug DC871F (N8079U), Ontario, CA. NR1 engine flameout inflight. Checked engine. Unable find cause.
- [Incident 19960213003639I](https://openairdocs.org/incident/19960213003639I), Feb 13, 1996: Doug DC871F (N8079U), Wichita, KS. Narrative: flight 329 (emery world wide) DC8 from lax to mgy diverted to ict with number 2 engine shut down. Aircraft landed without incident. Pilot report…
- [Incident 19920208032452I](https://openairdocs.org/incident/19920208032452I), Feb 8, 1992: Doug DC871 (N8079U), Miami, FL, Minor damage. Was struck on tail by N354AA that was departing on same runway. Aircraft had not cleared runway.
- [Incident 19780711043189I](https://openairdocs.org/incident/19780711043189I), Jul 11, 1978: Doug DC8/ (N8079U), Boston, MA. Landed with partial hydraulic failure. One hydraulic pump leaking, another with the shaft sheared.

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