kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
Aircraft
registration
31610
04-aug-05
F-HSEX
31560
1-Aug-05
PH-BQI
31557
27-Jul-05
PZ-TCM
31552
03-aug-05
PH-BQB
31550
02-aug-05
none
31538
30-jul-05
OO-TNB
Issued by :
Issued :
SPL/QA
September 08, 2005.
Description
Management Archive (CARMA). De Non-Conformity
heeft betrekking op het onvoldoende vertalen door de
afdeling Engineering van in AD notes gestelde eisen op
MRI’s, en taakkaarten, waardoor in de productie
beoordelingsfouten zijn ontstaan bij het catagoriseren
van uitgesteld werk. Ondergetekende heeft de reparaties
aan de betreffende wastecontainer acces doors op 03
aug 2005 fysiek gecontroleerd op het vliegtuig en daarbij
geen afwijkingen meer geconstateerd. Voor het
verlengen van het BVL van deze registratie heeft het
bovenstaande derhalve geen gevolgen.
Found transparent tape on the LH-side alternate static
port before starting leakcheck of the pitot/static system.
found at pfc and daily chk from brake assy pos 4 the fwd
brake wear ind gone and aft brake wear ind hanging
loose,fwd was already on ddl,when both are missing
brake must be replaced
No action description was made on AML M869
concerning reverser deactivation on engine 2. As a
consequence no reference was made to the Aircraft
Maintenance Manual.
In Manilla the lh Taxi light was found cracked. This was
en route deferred. In Amsterdam the taxi light was found
Covered with cardboard and taped with high speed tape.
The cardboard was almost completely burned away, and
the mounting flange/bracket was scorched. No CB's were
pulled. Altough the light was cracked, the fillament was
still working.
It seems that since approximately 25 july there are no
occurences reported. At least none have been printed or
received thru mail at both Duty Maintenance Managers
(WB+NB) desks This applicable for all a/c types !
After stabilised approach during landing flare, a/c
subjected to windshear, one main wheel touched down
before the otherand damage was caused to left main
Status
TIR
Feedback
Action
by:
OPEN
0
HF-WB
OPEN
0
USO-WB WILL INVESTIGATE WITH DECO
TEAM
CE WILL BE CONTACTED TO SEE IF THIS
IS A NORMAL SITUATION FOR A
RELATIVELY NEW BRAKE
MONITO
RING
0
Ground engineer will be contacted and issue
will be made part of CT
HF-LM
OPEN
TIR 05-163
will be investigated by HF-LM
HF-LM
CLOSED
0
0
CLOSED
0
Dat de occurrence mail niet doorkomt kan
kloppen, dat is een afspraak die is
voortgekomen uit een wens van MCC zelf.
Reden is dat MCC de meldingen alleen op
de printers wil krijgen. Dat de printers het niet
doen is gek. Daar hebben we een
spoedstoring voor aangemeld
OPERATIONAL INCIDENT. NO ACTION ON
KLM 145. OPERATOR INFORMED.
MSO
page 16 of 132
0
kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
Aircraft
registration
Description
Status
TIR
zonder dat ze gemerkt zijn met de critical task stempel
deze kaarten stonden ook niet op de criticaltask tally
sheet
Feedback
Action
by:
denken dat er wat geslipt is bij de PSG maar
gelukkig heeft deze oplettende gwk dit
herkend als een critical task en de juiste
aktie genomen, chapeau! Blijken trouwens
taakkaarten te zijn van EMDP, EDP en
supply filters verwisselingen en dus echte
critical tasks!
30831
10-jul-05
PH-BFD
Possible birdstrike during landing. Thorough visual
inspection of aircraft , no sign of damaged. Found in ams
during pfi lh inb aft flap nose area cracked.[see m844]
,caused by birdstrike in IAH.
OPEN
0
Birdstrike is een operationeel incident.
Wat ik me wel afvraag is of men IAH ook de
flaps heeft laten zakken om een inspectie uit
te voeren.
Met flaps "up" is het niet mogelijk deze
schade te zien.
0
30827
10-jul-05
ALL
0
0
0
0
30825
10-jul-05
all
0
0
0
0
30819
10-jul-05
PH-BPB
the pay of bonuses in areas where safety is an issue is a
bad thing. this can result in incorrect made decisions
safetywise.
It still appears to me that there are a lot of people who are
not actually responsible for the release to service of an
aircraft, are trying to influence the decision(s) that ground
engineers make in the dispatch. Some people are not
sensitive for this kind of pressure but I can understand
that others may break down easily. Given the fact that
safety and legal documents are the things we have to use
as wel as the fact that all other departments only have an
advising function, I would strongly advice to tell those
people not to apply this kind of practises. Some day this
will end in an disaster and we all know that the poeple
who have pushed us engineers, will deny any
involvements.
During OPC emergency lights acc Bow task CE83261,
noticed on rh side fuselage near aft flaps, emergency
light very weak.
CLOSED
0
Een paar maanden geleden hebben wij ook
een occ. gehad waar verkeerde lampjes in
de cockpit gemonteerd zaten bij de window
heat lights, deze kan daaraan toegevoegd
worden. Volgens het MEL 33-14-00 zou
zelfs de exterior emergency lighting u/s
0
Issued by :
Issued :
SPL/QA
September 08, 2005.
page 30 of 132
kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
Aircraft
registration
28327
22-Apr-05
PH-BFK
28326
22-apr-05
PH-BXH
28319
22-apr-05
PH-KCB and
PH-KCE
28311
22-apr-05
EC-IYI
28310
22-apr-05
PH-KCF
28264
20-Apr-05
PH-BQA
28252
20-Apr-05
PH-BDN
Issued by :
Issued :
SPL/QA
September 08, 2005.
Description
incorrect. lower redbar same problem. this all resultated
in stick shaker warning at fl300. speed indication on f/o
side was correct.
Catering at ams reported damage on wing to body fairing
rh side below door 22.
Found AD 2001-11-07 overdue on Motor-operated shutoff
valve PN EM 56-20 (Vendor Circle Seal). Subject AD is
effective from july 16, 2001 with compliance-time of 3
years, ending july 16, 2004.
During an occasional check on two MD11 aircraft on
Schiphol Centrum, I did the following findings on D151
type tourist class seats on MD11 aircraft: On several
occasions the bolt/nut connection of the Hydrolok to the
seatback was not according CMM 25-90-21 of the
specific seats. In many occasions there where wrong nuts
and/or wrong bolts fitted, Also washers where missing. In
total I found more than 10 nuts missing. In one occasion
de bolt dropped from the hydrolok (PH-KCE). I have
made contact with line maintenance on F pier, line
maintenance fitted a new bolt and nut. These aircraft had
both D-checks in China.
Wrong ipc used to find partnumber and so the wrong
partnumber is ordered and installed. Only
one(1)partnumber was ordered instaed of Two(2)different
partnumbers,left and right is different.
DEFECT: DURING ENG START LEVEL 1 ALERT HYD
PUMP TST FAIL.
During flt pax observed rh wing upper surface
movements , crew also inspected and reported same, on
advice MCC return back to SPL
Ref. AML M619, dd. 110305: Due to leakage of toilet
flush water in aft cargo compt. removed cargo loading
Status
TIR
Feedback
Action
by:
CLOSED
0
DAMAGE CAUSED ON OUTSTATION.
Dit is een van de eerste meldingen van
schade door belading, heeft verder
geen onveilige situatie opgeleverd ( verf
beschadigd). Voorlopig deze occurrence in
de trend volgen. Anders nog enige
awareness eraan geven door uitgave Flash
0
OPEN
TIR 05-082
UNDER INVESTIGATION QA
QA
OPEN
0
IT SEEMS WE NEED TO PUT MORE
ENERGY IN MANAGING OUTSOURCING
ACTIVITIES
HF-WB
OPEN
0
MORE ENERGY SHOULD BE PUT ON
MANAGING THIRD PARTY WORK
HF-NB
OPEN
0
0
HF-LM
OPEN
TIR 05-083
QA
OPEN
TIR 05-080
UNDER INVESTIGATION QA. UP TO NOW
NO INDICATION OF WHAT REALLY
HAPPENED
UNDER INVESTIGATION QA
page 77 of 132
QA
kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
Aircraft
registration
27035
8-Mar-05
PH-BDW
27031
8-Mar-05
PH-BFU
27030
8-Mar-05
PH-BDW
27019
7-Mar-05
PH-BDW
27018
8-Mar-05
PH-BXL
26959
06-mar-05
PH-BDO
26929
3-Mar-05
PH-KCB
26928
4-Mar-05
26927
4-Mar-05
Issued by :
Issued :
Status
TIR
Feedback
Action
by:
CLOSED
TIR 05-035
TIR REPORTED FOR STATISTICS
0
OPEN
0
MSO
MONITO
RING
0
MONITO
RING
0
Komt veelvuldig voor, probleem zal worden
voorgelegd aan Engineering om een
structurele oplossing te zoeken.
ALSO MANY THANKS FOR
OCCURRENCE, WELL OBSERVED. WILL
BE MADE PART OF CT
VERY GOOD OCCURRENCE REPORT.
WELL OBSERVED. WILL BE MADE PART
OF CT.
CLOSED
0
ADMINISTRATIVE PROBLEM.
0
CLOSED
0
0
MONITO
RING
0
PH-BFA
De-icing required according ground engineer. No
information from flight crew on the ATL action side about
start time, fluid-type used or mix-ratio. Open entry is not
released on outbound station, at SPL 2 days later the
entry is closed.
DD was not entered in MSF so no telex went to stations.
Occurrence is op verzoek van QA gemeld
door de EUR-DMM, waarom dus niet op de
dag dat het gebeurde vragen we ons af.
ATL entries: M584/585/588/589/590/591. QA
heeft Grd. Services gevraagd het
schaderapport op te sturen. Het voorval is
veroorzaakt door gebrekkige communicatie
tussen cockpitcrew en truckdriver.
CAPTAIN SHOULD HAVE REFERRED TO
DE-ICING IN ATL
OPEN
0
PH-BFA
LIGHTS ; FOUND FLOOR PROX LT AT SEAT 28ABC -
CLOSED
TIR 05-029
SPL/QA
September 08, 2005.
Description
release system as alternate extension)
found wrong type of lightbulb installed in the flightdek
emergency dome light. the partnumber installed was a
1308 (28 v)iso 1317 (6v)
Fire Prot/ equipm : occurence report : main deck cargo
smoke separation shield lh inbd decompression panel
found in open position .
APU air check valve is touching angle assy above the
check valve. 05-M5003/ 817552/ 028457
LH Wing, Krueger Flap 2 leading edge cavity area.
Pneumatic pipe line for water system pressurisation
which is clamped to wing anti ice duct is touching slat
hydraulic line just outboard of wing landing light. Also
check nut is loose where pipe line passes through rib
installation going inboard. 11-M5013/ 817301/ 028457
Anti skid box removed from BXL to serve BXK. Removed
unit 680294 with x-label 1357986. Apperntly unit not used
for BXK and got lost at schiphol centrum. Found a unit
installed in BXL without log of maintenance action.
Traced part/serie number of unit and found installed on
BXC.
A/C rolled forward after pushback track disconnected and
hit truck with nose gear.
De cockpit crew is zo te zien waarschijnlijk
vergeten de slip in te vullen
WILL BE ADDED TO TREND DATA FOR
0
0
HF-LM
HF-LM
page 105 of 132
0
kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
Aircraft
registration
26429
Enkele
dagen
geleden
?
26428
15-feb-05
PH-BFC
26427
15-feb-05
PH-BTA
26416
15-feb-05
PH-MCF
26400
15-feb-05
PH-BFN
26391
8-Feb-05
PH-BZG
26333
13-Feb-05
PH-BFF
26302
11-Feb-05
PH-KCG
Issued by :
Issued :
SPL/QA
September 08, 2005.
Description
oil leakage if engine was started.
Na in-taxie-en bij gate werden motoren uitgezet, maar
bleef beacon lt branden. Personeel dat vliegtuig afhandelt
bleef op afstand, blokken werden niet geplaatst. Iemand
in de gate met geel hesje gebaarde de cockpit crew dat
de blokken er lagen, waarop de brakes werden
gereleased. Vliegtuig rolde daarop 4 mtr naar voren.
GWK die wilde inpluggen moest wegspringen.
INCIDENT Tijdens intaxie-en op F4 was opstelvak voor
vliegtuig niet vrij van grond-equipment. Nacelle motor 1
raakte container of bagage-kar (waren niet bij ongeluk
aanwezig). Persoon die visual docking systeem bediende
heeft noodstop bedient om erger te voorkomen.
floorfittings from girdbar at lh fwd entry door where
incorrectly installed. (180 degrees turned)
found during wheel change #15 one brake disc all pins
missing and disc broken in two.
FLIGHT COMPARTMENT FWD OF LDG CONTROL
HANDLE MODULE P2-3 (BS 270/RBL 7.23/WL 332.14):
LDG QAUDRANT FASTENER NUT (REF.IPC 32-31-6601 ITEM 120) AT BEGINING OF THREAD (OF MOUNT
BOLT) - SUSPECT NOT TO BE FASTENED BEFORED.d 26-JAN-2005 AFT cargo compartment lining was not
repaired, but cargo was still carried for three fligths, this is
not in accordance with the MEL. NWA report was filed.
Smoke Separation Shield Main deck Cargo most Lh
outbd decompression panel found in open position.
PH-KCG staat met klachten in buitenland, onze PH-KCE
moet spare main-battery & battery-charger meenemen.
Er is echter maar 1 battery besteld terwijl de batteries als
paar verwisseld moeten worden. De 2e accu komt uit
H11, maar er is geen runner die hem brengt. Of wij hem
willen brengen wordt door LMO-er gevraagd. In H11 bij
magazijn blijkt dat er geen ADR-formulier (vervoer
gevaarlijke stoffen) is, daarom neemt runner battery niet
mee. Batterijen en charger naar vliegtuig, geen papieren
aanwezig, batterijen mogen zo niet mee. We worden naar
Status
TIR
Feedback
Action
by:
OPEN
0
0
MSO
OPEN
0
0
MSO
OPEN
TIR 05-023
0
HF-NB
CLOSED
TIR 05-021
INFORMED OPERATOR MARTINAIR
0
OPEN
0
uitzoeken
HF-LM
MONITO
RING
TIR 05-020
THE SUBJECT MEL WILL BE COVERED
BY CT.
WOO
MONITO
RING
0
MSO
CLOSED
0
WOO; regelmatig voorkomend probleem,
zullen naar structurele oplossing moeten
zoeken.
Het lijkt erop dat een niet hiervoor
geautoriseerde medewerker iets probeert te
versturen en daar niet de geeigende
procedures volgt. Het antwoord is dan ook
dat technici helemaal niets (zeker geen DG)
moeten vervoeren buiten het technisch
areaal en daarvoor de expedities of
magazijnen moeten raadplegen.
De DG WPI's van CS: 130010, TW130020,
page 115 of 132
0
kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
26017
2-Feb-05
Aircraft
registration
PH-BXG
25978
30-Jan-05
PH-BTG
25950
31-jan-05
PH-BXG
25945
30-jan-05
PH-BTA
25941
29-Jan-05
PH-BTH
25925
30-Jan-05
PH-CKC
Issued by :
Issued :
SPL/QA
September 08, 2005.
Description
After H-visit on 01-feb-2005, aircraft was transported
outside H10. Noticed APU fire extinguisher has low press
agent light illuminated. After troubleshooting found plug
D48080P has internal continuity between contacts and
therefore APU fire extinghuisher was discharged. Plug in
very bad shape.
Hil m660 29 jan 2005.RH runwayoff light cb
popped.Replaced rto light on m672.Found wrong lamp
installed 4554 iso 4551.Acc ipc l331,install pnr 4551. On
m680 the engineer suggested the there was a wrong rto
was installed and installed a new lamp. Both lamps where
replaced on the same station mxp.
After de-icing at OTP, crew performed full flight control
checks after pushback. During check flaps failed to
extend beyond 24 degrees. Initial trouble shooting
showed failure in flap load relief circuit.
During maintenance main rudder pcu was disconnected
from rudder. The hydraulic shutoff valves in the tail
compartment were in a position between the open and
closed position. For maintenance safety, they should
have been completely closed... Hydraulic pressure was, if
flight control switches in flight compartment were placed
in the "on" position, available for the main rudder PCU.
This probably happened and resulted in a damaged
rudder pcu and damage to the rh vertical beam of the
vertical fin. No danger tags were placed in the flight
compartment. The bolt which connects the main rudder
pcu to the rudder was u/s and a new one was ordered
aog. (job interrupt jc 08-M5010)
Landing gear: found during inspection at lh main landing
gear, upper drag strut mounted 180 degrees wrong.
upper fuse pin mounted now from outboard to inboard.
DEFECT: DURING CLIMB OUT AFTER +- 10MIN LOUD
BANG FROM BEHIND COCKPIT. DELTA-P WAS 7.0
PSI. 2ND BANG AFTER 15 MIN DELTA-P 8.3. 3RD
BANG AFTER 26 MIN DELTA-P 8.3 PSI. SOUNDS LIKE
THERE IS SOME TENSION IN THE AIRCRAFT
DURING CABIN - PRESSURE CONT OF M994: BUILT
Status
TIR
Feedback
Action
by:
0
MONITO
RING
0
SHORT CIRCUIT IN PLUG.PLUG WILL BE
INVESTIGATED. MANY THANKS FOR
OCCURRENCE REPORT.
CLOSED
0
PLEASE CONSULT MANUALS FOR RIGHT
P/N.
0
CLOSED
0
ISOLATED CASE.
0
MONITO
RING
0
Hydraulic Shut off valves can be opened
involuntarily. WE consider issue of an Aircraft
Safety FLASH.
HF-NB
CLOSED
0
0
OPEN
0
180 GRADEN VERKEERD OM MONTEREN
KAN. IS BIJ TOEVAL NA MAANDEN PAS
ONTDEKT.
FLIGHTCREW HEEFT EERSTE TWEE
VOORVALLEN NIET IN BOEK GEZET! KIST
HEEFT ER TWEE KEER MEE GEVLOGEN.
MSO NEEMT CONTACT OP MET
ENGINEERING. HF LM NEEMT CONTACT
OP MET FLIGHT.
MSO
page 122 of 132
kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
Aircraft
registration
25923
30-Jan-05
PH-BFC
25922
30-Jan-05
PH-CKB
25917
29-Jan-05
PH-OFD
25915
28-jan-05
PH-BTA
25914
28-Jan-05
ph BFO
25910
28-Jan-05
ph-bfg
25865
27-Jan-05
EI-CUA
Issued by :
Issued :
SPL/QA
September 08, 2005.
Description
UP ALSO REPORTED BY CREW OF 9182 HKG-DXB
ON 26TH JAN AND BY CREW OF 9168 SIN-DXB ON
30TH OF JAN.
HERAM: Afgelopen week 3x meegemaakt dat equipment
uit gereedschapsmagazijn VOC ontbreekt. 1) loodjestang om brandblusfles van nieuw zegel te voorzien was
weg (missing) 2) push-pull unster om flightcontrol klacht
te controleren acc. MAI was weg (missing) 3) loep om
crack te inspecteren was weg (missing.
During PFI today, found complete paperwork of H-check
27 jan 05 (BOW-AMS-CKB-27jan2005-1) in cockpit
cabinet.
Fuel was leaking out of the rh wing wingroot vent
drain.Flame arrester valve was stuck open and a nock on
the valve made it reseated and stopt the fuelleak.
During rebuild of cockpit due to MO53-0351 found both
EHSI's missing. Could not find any paperwork regarding
the removal of both EHSI's. After check in
COMPAS/CROCOS system found both units to be
removed from aircraft on 31-dec-2004.
Tijdens FA NFDE gevonden op densito meter van HST
tevens uitgesteld werk van 21 juli 2004 met zelfde klacht
en daarbij stond RA 495087 ingevoerd NRC 08M5001
M.a.w. kist vliegt al een half jaar met een NFDE en die
lossen we niet op omdat er geen onderdelen besteld
worden. Er was ooit beloofd dat dit gecoverd zou worden
dat RA's wel op tijd geleverd en of besteld worden. Bij
andere mijen is dit echt niet mogelijk
Diverse AMM verwijzingen op de taak kaarten in de FC
zijn niet terug tevinden in M-BOX. BV: operational check
of: forward cargo container compartment acc amm 25-5300/575 ff par 76 and 77 post mo 25-2718b. Bij navraag bij
CE moet er een light weight lowerdeck cargo handeling
system-test uitgevoerd worden. Een operational check is
niet het zelfde als een system test. Door dat de tekst niet
klopt en de amm verwijzing niet te vinden is worden
verkeerde testen uitgevoerd.
According minutes of meeting 07 dec 2004 written by Mr.
Status
TIR
Feedback
Action
by:
OPEN
0
Hf-LM zal contact opnemen met VH .
HF-LM
CLOSED
0
Indidenteel.
HF-LM
CLOSED
0
DOORGEGEVEN AAN CITYHOPPER
0
CLOSED
0
PROCEDURE MBT KANNIBALISATIE IS
NIET GOED GEVOLGD
0
OPEN
0
LIJKT OP EEN PROBLEEM MET
WERKVOORBEREIDING; ER IS EEN WPI
VOOR MONITOREN UITGESTELDE NON ROUTINE. KOMEN WE OP TERUG.
HF-LM
MONITO
RING
0
M-BOX PROBLEEM. ZAL WORDEN
OPGENOMEN MET
ENGINEERING.SPL/CC3 ( AMP groep)
heeft dit specifieke geval aangepast, rest van
de M-BOX problemen is men doende om het
in te plannen
MSO
MONITO
0
Een duidelijk voorbeeld van het niet goed
0
page 123 of 132
kem
QUALITY ASSURANCE – SPL/QA
SUMMARY OF REPORTED OCCURRENCES 2005
Number
Date
Aircraft
registration
25835
25-Jan-05
N/A
25832
26-Jan-05
PH-BFW
25821
25-Jan-05
PH-BXK
25788
24-Jan-05
5Y-KQZ
Issued by :
Issued :
SPL/QA
September 08, 2005.
Description
Status
X. At point 2 procedures annex A blue panorame has no
regulation about double inspection items. At point 3
procedures annx B blue panorama allows KLM E&M to
perform work according KLM procedures. This also
means duplicate inspection as mentioned in KLM
appendix c. According maintenance management
&organization exposition(MMOE) of Blue Panorama part
2.23 control of critical task: at point 2.23.2 taks about
additional inspection items(double inspect)witch is more
than what KLM E&M has stated in there Appendix C for
duplicate inspect. At blue panorama it also includes
powerplant/landing gear and airframe structures(see
MMOE 2.23.2 of Blue panorama) this problem is mention
at the project supervisor
Found in H14 bay 1 again 2 cylinders used for
compressed gas filled with not " DRY NYTROGEN" but
with AR/CO2. Only " DRY NYTROGEN" may used in the
hangar.
A/C TOOK OFF AT AMS WITH NO AIRSPEED AND ALT
INDICATIONS ON CAPT SIDE (ADC-L). (T/O WAS NOT
ABORTED??) AFTER SWITCHING CAPT SIDE TO
ADC-C ALL IND NORMAL. IN ORD THEY FOUND
PITOT / STATIC CONNECTORS NOT CONNECTED ON
ADC-L. (ADC-L REPLACED ON M953 / 25JAN05)
REMARK: IS IT ALLOWED TO MAKE A T/O UNDER
THESE CONDITIONS??
Found during inspection at nose landing gear, lower
torsion scissor hit by towbar less towing truck at lh side,
mid part of torsion scissor 23-01-05 at d18. This aircraft
was the spare aircraft used for PH_BXD which was hit by
a bagage truck.
Upon arrival it was noticed that on the left engine two "do
not operate" tags were installed on the thrust reverser
doors. Only the most lower ones were installed. When
checking the Acceptable Defered Defect book no entry
was made of a deactivated reverser neiter were the two
control CB's pulled. When we asked the new crew they
were aware of a deactivated reverser but this could not
RING
TIR
Feedback
Action
by:
voorbereiden en op de hoogte stellen van de
P&P van een klant.
CLOSED
0
TRANSFER NAAR ARBO.
WOO
CLOSED
0
HF onderzoek uitgevoerd.Info bij HF-LM op
te vragen.
HF-LM
CLOSED
0
foto's zijn opgevraagd. Foto's zijn
doorgestuurd naar Ground.
0
OPEN
0
Op buitenstation is niet goed gedeactiveerd
en is ook het boordboek niet
bijgewerkt..betrokken GWK heeft een zeer
effectieve actie uitgevoerd via de Telex.
Operator zal op de hoogte gebracht worden
(via TQ)
MSO
page 124 of 132