MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
DATE A/C TYPE A/C REGISTRATION PAGE
B737 1 of 10
TITLE
“DAILY” CHECK
REFERENCE MEN MAN-HOURS DOWN TIME
EO B3-05-0001 5,30
3 5,50 for
winter period
DEPT/TEL NAME
ED/44-33-2 Averyanov
ITEM TASK/JOB DESCRIPTION MECH INSP
A1
1 PRELIMINARY
A. Make sure that the wheel chocks are in position.
B. Energize aircraft electrical circuits (AMM 24-22-00-860-811).
A1
2 WHEELS and TIRES INSPECTION
A. Check nose and main landing gear tires for proper inflation. Service as required.
AMM 12-15-51-610, 12-15-51-780 - MP 32-350-00.
B. Visually check nose and main landing gear tires and wheels for condition and wear. If tire wear
is within AMM requirements but the minimum depth of any groove is equal or less than 2mm,
then replace corresponding wheel (applicable to main base only). In case of wheel absence in
store, create AMOS WO (category "DD") to request replacement of the corresponding wheel
not later than next Daily Check. AMM 32-45-00-700, MP 32-360-00 (CAD OWO 01072019NVV01)
3 MAIN GEAR BRAKE WEAR PINS (CAD OWO 01072019NVV01)
A. Perform general visual inspection (GVI) the brake wear pins for minimum extension. The wear
limits are following (for at least one wear indicator of each brake):
1) for Daily-check at SVO as part of "S-check" or higher checks: 1mm or less.
2) for Daily-check at SVO as a single line maintenance check or outside SVO:
level with or below the face of a guide and at the same time if it is equal to or less than
1mm, create an AMOS WO (category "DD") to request replacement of the corresponding
brake not later than next Daily-check at SVO. AMM 32-41-41-700-801 -
B. Check brake units for leakage.
A1
3.C Perform 3.A and 3.B on the left MLG. MP 32-270-01
A1
3.D Perform 3.A and 3.B on the right MLG. MP 32-270-02
A1
4 SHOCK STRUT CLEANING
A. Clean exposed surfaces of the left and right main landing gear shock strut, AMM 32-00-10-
100-802 - MP 32-010-01, 32-010-02.
B. Clean exposed surface of the nose landing gear strut, AMM 32-00-10-100-802 -
MP 32-060-00.
Revision 0 Form 2.13.7/1
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
2 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
5 ENGINE OIL
A. Perform oil level check of engine № 1 and № 2 (Ref. AMM TASK 12-13-11-600-801)
CAUTION: DO THE “REPLENISH THE ENGINE OIL” PROCEDURE BEFORE THE OIL TANK
BECOMES COOL (60 MINUTES AFTER THE ENGINE SHUTDOWN). IF THE TANK
IS COOL, YOU CAN FILL IT TOO MUCH AND CAUSE AN INCORRECT
INDICATION OF THE OIL CONSUMPTION RATE.
Do a check of the oil quantity with the sight gage.
If the oil level is below the full mark, add engine oil to the gravity fill port of the oil tank and
stop before the full mark of the sight gage.
B. Calculate oil consumption for each engine after oil replenishment (Ref. AMM SUBTASK 71-
00-00-910-025-F00).
Oil quantity refilled (quarts/gallons/liters)
Oil consumption per flight hour =
Last leg flight hours
Normal oil consumption is less than 0.4 US quart/hour (0.38 liters/hour).
NOTE: You must RECORD oil consumption for engines in ATLB (“REPORT” box) and use the
fault isolation manual (FIM) if one of the following conditions occur:
The oil consumption shows a gradual increase.
The oil consumption shows a sudden step increase.
The oil consumption is more than 0.8 US quart/hour (0.76 liters/hour).
B1
C. Perform oil level check on engine № 1.
B1
D. Perform oil level check on engine № 2.
A2/B1
6 CREW OXYGEN
Make sure the pressure shown on the pressure gage (oxygen panel P5) is above the minimum
pressure necessary for dispatch (AMM 12-15-21-210-801-002) for 3 crew members.
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
3 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
A3
7 EMERGENCY EQUIPMENT
Detachable Emergency and Safety Equipment is stowed in the flight and passenger
сompartments. Placards in the airplane mark the location of these items.
A. Perform Detachable and Safety Emergency Equipment Check for presence, proper installation
in accordance with Figure 1. Do actions to rectify discrepancies, in case of equipment missing
or damaged. Use AMM TASK 25-64-00-210-802 for Detachable Emergency Equipment Visual
Check.
B. Check the seal and expiration date on the First Aid and Medical kits. If the seal is broken or
date expiry, replace kit. The First Aid Kit or Medical kit must be replaced not later than 3 days
before the expiration date. MP 25-420-00, MP 25-430-00.
C. Perform Service Inspection of Flashlights.
1) Ensure the tamper shield is mounted and secured properly.
2) Ensure the LED is flashing at an interval of approximate five seconds, and that it can be
seen easily in normal lighting conditions.
D. Perform inspection of portable oxygen bottles iaw AMM 35-31-00/601.
1) make sure that the pressure gauge control seal isn't damaged,
2) make sure that the pressure gauge control seal is located on the center of the dial,
3) make sure that the pressure gauge arrow is not bended or deformed.
4) Pay attention to the oxygen mask connection outlet position (see Figure 2).
5) Check oxygen masks for presence, condition and proper installation (see Figure 3).
NOTE: minimum acceptable pressure for a/c departure is 1500 psig at the air temperature of
21 °C.
WARNING: DO NOT USE PHISICAL FORCE TO CHANGE OUTLET POSITION!
Figure 2
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
4 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
OXYGEN MASK POSITION OXYGEN MASK ON CYLINDER APPROXIMATELY AS SHOWN, WITH A
INSTALLATION MINIMUM OF 1.0 INCH CLEARANCE FROM THE LATCH. FOLD THE CARRY STRAP INTO
APPROXIMATELY 5.0 INCH LONG FOLDS. SECURE MASK AND CARRY STRAP TO THE
CYLINDER WITH VELCRO. BEFORE INSTALLING VELCRO, HOLD THE END WITH THE
PILE SIDE TOWARDS YOU, FOLD END UNDER TWICE TO CREATE 1.0 INCH SQUARE
"TAB". INSTALL WITH PILE SIDE OUT AND CUT, MAINTAINING A 2. 0 TO 4.0 INCH
OVERLAP. THE "TAB" SHOULD BE TO THE SIDE OF THE OXYGEN CYLINDER. WHEN
MULTIPLE OXYGEN MASKS ARE REQUIRED, THEY MAY BE INSTALLED EITHER
SEPARATELY OR ON TOP OF EACH OTHER WITH A SINGLE PIECE OF VELCRO.
Figure 3
E. During fire extinguisher inspection make sure that wire seal is not damaged.
F. Make sure that each demo kit consists of demo safety belt, demo oxygen mask and demo life
vest.
G. Check the presence and condition of the onboard wheelchair, stowed at FWD full-height closet
integral to Galley G2.
H. Check crew life vests located at the lower stowage compartment of attendant seats for
presence, condition, proper installation and proper attachment (see Figure 4). If life vest (life
vest wrap) and/or life vest strap is missing, torn, damaged or dirty - make corrective actions.
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
5 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
Figure 4
PASSENGER COMPARTMENT CHECK A3
8
(AT MAIN BASE ONLY)
Perform visual check of passenger compartment for serviceable, clean and presentable
conditions including lavatories, galleys (ovens, coffeemakers), PSU, passenger seats, floor
covering, curtains, class dividers, OHSCs, its doors and sidewalls.
A1
9 HYDRAULIC
Check that hydraulic quantity indications in cockpit (CDS) show 92 % or above. Do a Hydraulic
Reservoir Servicing (AMM 12-12-00-610-801), if necessary. Do not overfill reservoirs.
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
6 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
A1
10 FUEL SYSTEM SAMPLING
Perform fuel system sampling for each fuel and surge tank. There are five sump drain valves in
total, installed on the airplane (AMM 12-11-00-680-801).
ATTENTION TO MAINTENANCE PERSONNEL!!!
According to Russian FATA order 7065/03, dated 21.02.2020, any unusual contamination (e.g.
jellylike substance, powder, or other) that is found in the drained fuel, must be considered as
affecting the aircraft safety operation. If the contamination is found, save the fuel samples and
contact AFL Flight Safety Department (e-mail: bp@aeroflot.ru, phone: +7(495)753-81-63, NEC:
41010) for further instructions, before next flight.
A1
11 WEAPON BOX
Check Weapon Box and two tie-down straps AIC0309-A03 (1 ea.) and AIC0309-A04 (1 ea.) or
alternative in aft cargo compartment for presence and serviceable condition.
A1
12 FLYAWAY KIT (AT MAIN BASE ONLY)
A. Check Flyaway kit for presence in aft cargo compartment.
B. Check content of Flyaway kit i.a.w. list below. Make an order (Material Request) if any item is
missing; open corresponding WO in IT-system with status “DM”.
№ Part description Qty PN
1 PIN – DEACTIVATION 4 315A2258-2
2 LOCK PIN - NOSE GEAR STEERING VALVE 1 A09003-2
LOCK PIN - THRUST REVERSER ACTUATION
3 1 C78004-1
MODULE, contains (2) C78004-2 pins
4 TOWING EYE BOLT ASSY 2 F72719-500
5 COVER, pitot 5 KPC3-480-325
See AMM 10-11-01-580-
6 COVER, engine inlet 2
801
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
7 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
A1
13 LANDING GEAR DOWNLOCK PINS
A. Check presence of three (3 ea.) downlock pins on the landing gears or in the cockpit (the bin
over the coat stowage).
B. Check condition of streamers with split rings. Replace streamers if it worn or heavily
contaminated: original PN NAS1756-36 or alternative PN AIC0881-A03 (for NLG) and
AIC0881-A04 (for MLG).
FWD AND AFT CARGO COMPARTMENTS AND A1
14
DOORS (to be done from 01 October till 30 March)
Perform the following to prevent FWD and AFT cargo compartment and doors freezing:
NOTE: DURING COLD WEATHER, DO NOT OPEN THE CARGO DOORS IF IT IS NOT
NECESSARY.
NOTE: USE NATURAL RUBBER (LATEX) GLOVES FOR THIS WORK.
A. Open FWD and AFT cargo compartment doors.
B. Apply by brush or by lint-free cotton cloth a small amount of anti-icing fluid complying with
SAE AMS 1428 standard on these areas:
1) handle and exposed latching mechanism
2) lower door sills
3) bottom edge of the door
C. Close FWD and AFT cargo compartment doors.
FWD AND AFT CARGO COMPARTMENTS A1
15
(CAD OWO 20210712KIE01)
Visually inspect all cargo compartment internal surfaces (scuff plates, lining, floor structure, all
floor panels and sidewall panels, etc.).
If damage or repair recorded in AMOS, please check if marking P/N ST-2021-0001 is
installed.
If marking is not installed, please install marking accordingly.
If identified damage or repair is not recorded in AMOS, follow technical documentation for
assessment and repair. After assessment or repair accomplished, please add information
into AMOS and install marking P/N ST-2021-0001 in accordance with AMM B737 20-10-
11-400-801 with maximum distance 50 mm away from identified repair or damage.
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
8 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
CHECK PLACARDS IN THE ACLB A3
16
(AT MAIN BASE ONLY)
Check presence and quantity of “DO NOT USE” and “INOP” placards in the actual ACLB
(CAD OWO 20210623ZDA01):
AIC0575-P02 or AEM-0705-8002 – 2 ea.,
AIC0575-P01 or AEM-0705-8001 – 2 ea.,
AIC0592-P02 or AEM-0705-8003 – 2 ea.,
AEM-0702-1212 – 2 ea.
Complete this set every time when quantity is not enough.
А2/B1
17 CHECK PRINTER PAPER (AT MAIN BASE ONLY)
Push the SLEW switch to make sure the printer has paper.
NOTE: If the edge of the paper shows a color, there is not sufficient paper in the printer.
If there is not sufficient paper in the printer, install paper in the printer (Printer Paper
Installation, TASK 31-33-01-400-802).
B1/B2
18 FINAL WORKS
A. Check that all circuit breakers, except of deactivated systems, are closed.
B. Ensure all passenger/crew doors, cargo compartment doors, service panel doors and avionic
doors are correctly closed and locked.
C. Install protective covers and perform parking procedures, as necessary (AMM 10-11-01-580-
801).
D. De-energize aircraft electrical circuits (AMM 24-22-00-860-812).
E. Issue CRS for “DAILY” check in ATLB.
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
9 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
Figure 1, sheet 1: Emergency and loose equipment
Revision 0 Form 2.13.7/2
MAINTENANCE JOB CARD WORK No: B3-05-0001 rev 19
A/C REGISTRATION PAGE
10 of 10
ITEM TASK/JOB DESCRIPTION MECH INSP
Figure 1, sheet 2: Emergency and loose equipment
Revision 0 Form 2.13.7/2
