FIELD TRIP
REPORT
OPERATION DESERT DEEP FREEZE
T1 Minimum
Control Speeds
Edwards Air
Force Base
Lancaster, CA
USA
19.-23.
December, 1998
by
Anthony Tellier,
as told to Cyrus Jackson
BRR B717 Flight
Test Team
Yuma, AZ USA
The Boeing 717-200
“717XA” (a.k.a. “T1”) flew to Edwards Air Force Base on Friday the 19th of
December 1998 to perform Minimum Control Speed tests (“Vmcg”). Edwards is located in the so-called “High
Desert” of Southern California on the margins of Rogers Dry Lake. Rogers, once known as Muroc Dry Lake, has
been the site of several Space Shuttle landings. Edwards is the USAF Flight Test Center and where Chuck Yeager
first broke the speed of sound.
The Vmcg
testing was severely compromised by the strong west winds that arose at dawn --
and blew all day and into the night — for several days in a row. The test wind limit was only five (5) knots
and the crosswind component was a small two (2) knots. The 25-knot winds (gusting to over 30 knots
at times) easily exceeded those limits, precluding any such testing. Maneuver and Control Stability work was
performed as a fill-in.
Vmcg
tests require the high-power “chop” of one of the engines, which results in a
flow reversal, a strong “Boom” and an airframe shudder. Boeing asked that the HPC and LPT be
borescoped at the end of each day’s Vmcg testing. Borescoping and videotaping in the field
proved to be somewhat “difficult” under the conditions at Edwards during this
Report time frame. The weather was
cold. The weather was windy and the
days were the shortest of the year. It
snowed one evening. The heater in the
Lancaster motel went off-line. You had
to put your beer in the reefer to keep it from freezing.
The three
borescope series that were performed showed both engines’ hardware to be in
good condition.
HARDWARE PROBLEMS
The
Boeing-required, daily, visual inspection of the igniters resulted in two parts being broken at the wrench
flat during their re-installation. BRR
records indicate that each particular igniter plug had been removed and
replaced for these inspections as follows:
13104;
outboard, #1, starboard side, right [ALF] — nine removals. FRACAS 1444.
13105;
outboard #1, starboard side, right [ALF]) — ten removals. FRACAS 1443.
The thin wall of
the igniters’ shell was broken in two, brittle pieces, held together only by
the ceramic core, suggesting a low-cycle fatigue situation. (A Boeing calibrated torque wrench is used
to install the igniters per “74-20-04-420-001 A. (4)”: 250 Lbf-in). Evidence shows that Boeing had used a
colloidal copper anti-seize compound (often referred to by a brand name
“Never-Seize”) on the igniter threads.
The BRR Maintenance Manual specifies only the use of simple turbine engine
oil. It was not possible to fully hand-install
the RH 13105 igniters into the burner case bosses. (Note: This reported increase in run-on torque has not
been taken into account at installation.)
(Note:
Previously, in Yuma, another oft-inspected igniter was destroyed in the same
manner. FRACAS 1439.)
The igniter
replaced in 13105 #1 provided an excellent baseline for observing the erosion
from Continuous Ignition. Installed
brand new, S/N 752, was operated for a maximum of 37 minutes of continuous
ignition and sustained 0.028-in center electrode erosion and an 0.008-in
increase in diameter across the firing tip.
Although this is but one snapshot of the phenomenon, it suggests that
the maximum erosion of 0.12-in would be reached at or past the 10-hour limit of
continuous ignition. Under this severe
condition, the igniter’s tip is melted away; balls of molten metal can be found
on the rim and the center electrode.
The standing
requirement for a daily visual inspection and measurement of the igniters’ tips
was rescinded, by Boeing, on the evening of 21st of December. However, these inspections are still
required prior to and after any single-engine flying or any otherwise
continuous ignition operation.
The requirement
to borescope the HPC after
any low-power start-up surge was (thankfully) rescinded as noted in Flight Test
Report #104 (717LB104_21Dec98):
During
the initial (‘cold’) start prior to flight 125 of aircraft T1 the LH engine
(S/N 13104) surged once again on closing of the stage 8 HBV. Ironically the LH
engine on aircraft T2 (S/N 13107) surged as well during the first start of the
day some 30 minutes later (T1 being at Edwards, T2 at Yuma). After discussions
with the pilots and the Boeing Management (present at Yuma), it was decided to
waive the previously required HPC borescope inspection, if the start surge can
be clearly attributed to the known stall margin problem during stage 8 HBV
closure. After review of the PWM data both aircraft were cleared for flight,
hence minimizing the delay to the test program.
(We looked at
the Stage 3 blade TE s so often that we are now close friends.)
Three (3) Core Fairing Panel “Tridair” Fasteners
were replaced due to cracking at the threaded end: two (2) on Engine 13104 and
one (1) on Engine 13105. FRACAS 1448.
Three (3) Bypass Duct Access Panels were
found to have minor de-bonding at the corners of the Kevlar™ acoustic
material:
Engine 13104
Large
Panel P/N BR715APA002-01, S/N 3112V022 -- 4 inches
Small
Panel P/N BR715xxxxxx-xx, S/N x112Vxxx -- 2 inches (complete part info was
obliterated)
Engine 13105
Large
Panel P/N BR715APA002-01, S/N 3112V016 -- 2 inches.
(Note: These
panels are not (necessarily) re-installed in the original or previous location
not in the prior orientation.)
Their
condition was considered minor based upon parts previously seen in Yuma and at
Chula Vista. The parts were
re-installed and will be re-inspected back in Arizona. Flight Test suggests that a written
"Pass-Fail" inspection criteria for the acoustic material's bonding
be provided.
LESSONS LEARNED
Facilities
The
pad where the B717 was positioned -- "Building 1830” -- had no
facilities. We were able to borrow a
small hydraulic lift -- a C-17 work platform.
We needed more (and better) ladders.
We obtained 110vac power from the 717.
Lighting was by a drop-light and flashlights. We could have used more.
Extension cords are necessary items.
Contrary
to popular opinion, the aircraft was not (repeat "NOT") in a hangar
but positioned outside, subjected to all of the elements. Out there we experienced all of the human
emotions,
Borescoping
Invasive
inspections should be limited to an absolute necessity in the field. The possibility of self-induced,
flight-restricting problems is greater under such adverse conditions and with
limited support.
Handling
small parts with, or without, gloves is tricky, at best. While items were dropped, they were found.
The
borescope kit should have an extension cable for the recorder, similar to the
one provided for the monitor. The short
lead that is now with the set-up is too short when the recorder/viewer is
resting on the lower engine cowl. Due
to some ambient light conditions, the recorder's monitor can be very difficult
to see. A black cloth, like a portrait
photographer's, should be used.
Fly-Away
Kits
All three test aircraft -- T1, T2 &
T3 -- should have a Fly-Away Kit permanently on board. A simple toolbox would suffice. It would have lettered on it: “BRR Fly-Away Parts Kit”. Tip: Each engine’s build records should be
consulted in order to determine which of the seven sizes of Adjusting Washers
is peculiar to each igniter location and the appropriate spare washer placed in
the kit.
The
“Kit” boxes would be locked with one of a set of Master™ keyed-alike
padlocks. The keys would be distributed
to all mechanics and the various crew chiefs.
Nothing should ever be taken from these kits except while in the
field. A checkout list would be inside
the toolbox and diminished stocks replaced upon return to Yuma.
Fly-Away Parts Kit
Core
Panel Fasteners & Washers Long
and short
Filter,
Oil QA07520
Filter,
Fuel -- Motive Flow QA07861
Igniter
Washers (7) BRR17953-59
(Ref: Engine Ass’y Records)
Igniters
w/ CoCs (4) Y242-5
Igniter
Boss
Igniter
Boss Seal(s)
O-Ring, AS43013-118
O-Ring, AS43013-122,
Small
O-Ring,
Filter -- Oil AS43013-153,
Large
O-Ring, AS43013-240
O-Ring, AS43013-241
O-Ring, AS43013-243
O-Ring, AS44066
THANKS
The
T1 crews of Bill Ellis and Abdon Herrera helped us complete the numerous
inspections. In particular we would
like to thank James Kitchen (on loan from T2), Mike Barrera and Kenny Lesch for
allowing us to use their aircraft "home" as a base of operation,
coffee bar and refuge.
USEFUL SITE INFORMATION
PULL OVER
The
EAFB Air Security Police will reportedly ticket anyone exceeding the posted
speed limits ... with no leeway; no “10%” cushion; no anything other than a
serious military-justice citation. The
Security Police are eighteen-year-olds with guns and power, a bad combination
at best. Use your cruise control! The Sierra Highway from Rosamond to
Lancaster is radar-patrolled by LA County and Kern County Sheriffs:
"County Mounties".
REMOTENESS
The
base is about thirty miles NE of Lancaster, through scenic Rosamond, off the
Sierra Highway via “Rosamond Road”.
(You can also take the "14" freeway from Lancaster at the
Willow Springs Raceway sign.) You will
have to stop at the Base gate(s) and identify yourself to the Airman. “Boeing Flight Test” and your badge will
suffice. A taxi ride, one way, will run
you well over $50 US.
During
the end of December 1998, due to “Operation Desert Fox”, they had (in
capitals):
THREATCON ALPHA
Be Cautious
Be Aware
Report Suspicious Activity
(This latter should have alerted the
authorities to the T1 crews!)
The
West Gate road to the Base is a straight, flat, four-lane, divided highway with
a oh - so - s l o w 60-mph speed
limit. The Base, and the long arm of
the Air Force law, actually extends westward past the (apparent) West Gate, so
be advised.
You
cannot drive onto the “Building 1830” Ramp without a military driving
license. Boeing T1 A/C Crew Chiefs Bill
Ellis and Abdon Herrera had them, however, and had to shuttle crews and
equipment to and fro.
WEATHER
Windy,
period. Cold. Real cold! Or hot. But windy no matter what.
LODGING
The
motels normally used by Boeing are in Lancaster some 30 miles away from
Edwards. Which is a drive made even
longer than it would suggest at first glance, due to the omniscience of those
pesky Security Police.
The
“The Inn Of Lancaster” has:
Breakfast
Coffee
maker
Microwave
Modem-friendly
phones and jacks (bring a multiple phone socket adapter and a phone cord. And perhaps an extension power cord and a
wall socket multiple adapter.)
Pool
Spa
TV
-- with lots of channels
VCR
Workout
room
A
terrific, low-peso, Mexican gritzo right next door
(805)
945-8771
(805)
948-3355 (Fax)
The
Inn Of Lancaster
44131 North Sierra Highway
Lancaster, CA USA 93534
The
motels in Rosamond, although but half the distance to the Base, are best
generously described as “seedy”. But
they are only half the distance.
With a Moose Lodge down the road ... you aren't going for the fun,
anyway.
BASE OFFICE PHONES & DOOR CODES
The
military mind has the phone system set up somewhat different than in the real
world.
Building
“1830A” Fax: (562) 593-1079 (In the MD C-17 area)
Building
“1830A” In Line: (805) 277-6868 + 2631/3/4/5/8
Building
“1830A” Out Line: 99 + A/C + Number (No “1” is needed or
allowed, OK?)
Building
“1830A” Door Combination: 4-18-30
Building
“1830A” East Fence Gate: 4-3-1
FOOD & STUFF
The
only thing that civilians can purchase on the Base is food. There is a Burger King (Hire The
Handicapped) near to, and a food mall in, the BX (Base Exchange). The Cactus Cafe ("Now Open") is close to the aircraft. You cannot purchase gasoline at the lone,
long-lined Base fuel station (except when returning the rental vehicle to the
Enterprise office on Base) ... or buy any of the discounted goods at the BX.
The
NASA Gift Shop has hats, mugs, shirts and things for civvies.
MUSEUMS
There
are some outdoor aircraft displays:
B-52
F-111
F-104s
F-8
(Fly By Wire)
F-8
(Supercritical wing)
F-84
HL-10
(Lifting body)
J-10
engine
J-79
engine (F-104, B-58, F-4, etc.)
J-93
engine (XB-70)
P&WA
engine (old!)
LLRV
(Lunar Landing Research Vehicle – w/ a vertically-mounted GE engine)
Mate-Demate
Device (puts a Space Shuttle onto the NASA B747)
Meteor
P-59A
(First USA jet plane, circa '42)
Saberliner
SR-71
(clapped out)
T-38
T-46
X-15
X-1E
X-29
DARPA/Grumman (Fwd-swept wings and canards)