Pro in Version B737 FAP-356 Pre-Purchase & Re Delivery Report FINAL

Aircraft Pre-Purchase & Redelivery Inspection Report

On Behalf of

ProInversion, Peru

Aircraft Type: B737-528 Aircraft Registration: FAP-356

International Bureau of Aviation

July, 2007 Page 2


Table of Contents

TABLE OF CONTENTS ...........................................................................................................2

SUMMARY ...............................................................................................................................4

PHYSICAL INSPECTION REPORT.........................................................................................5

1.1 Inspection Conditions ..................................................................................................................... 6

1.2 Physical Inspection.......................................................................................................................... 6 1.2.1 Aircraft Manufacturers Data Plate & Owners Data Plate ..............................................................................6 1.2.2 Fuselage ...............................................................................................................................................................6 1.2.3 Empennage..........................................................................................................................................................6 1.2.4 Wings, Flaps and Control Surfaces ..................................................................................................................6 1.2.5 Structure ...............................................................................................................................................................7 1.2.6 Landing Gear .......................................................................................................................................................7 1.2.7 Engines.................................................................................................................................................................7 1.2.8 Auxiliary Power Unit............................................................................................................................................7 1.2.9 Flight Deck ...........................................................................................................................................................7 1.2.10 Passenger Compartment ...................................................................................................................................7 1.2.11 Galleys and Lavatories.......................................................................................................................................9 1.2.12 Equipment Compartment .................................................................................................................................10 1.2.13 Cargo Compartments .......................................................................................................................................10

1.3 Conclusion ...................................................................................................................................... 10

AIRCRAFT RECORDS INSPECTION....................................................................................11

General Aircraft Description................................................................................................................ 12

Aircraft Utilisation................................................................................................................................. 12

Certified Operating Weights ................................................................................................................ 12

Maintenance Program .......................................................................................................................... 12

Maintenance Schedules and Status ................................................................................................... 13

Structural Significant Items................................................................................................................. 13

Titled Engines........................................................................................................................................ 14

Auxiliary Power Unit (APU).................................................................................................................. 15

Landing Gears....................................................................................................................................... 16

Fuel ......................................................................................................................................................... 17

July 2007 Page 3


Equipment and Furnishing .................................................................................................................. 17

Primary Overhaul Agencies................................................................................................................. 17

Deferred Defects ................................................................................................................................... 18

Aircraft Modifications and STC’s ........................................................................................................ 18

Airworthiness Directives...................................................................................................................... 19

Appliance and Engine Airworthiness Directives .............................................................................. 20

Aircraft Damage Chart.......................................................................................................................... 21

Hard Time Components Listing .......................................................................................................... 21

Documents List ..................................................................................................................................... 22

AVIONICS STATUS REPORT ...............................................................................................23

ATA Chapter 22: Auto Flight................................................................................................................ 24

ATA Chapter 23: Communication ....................................................................................................... 24

ATA Chapter 27: Flight Controls......................................................................................................... 25

ATA Chapter 31: Independent Instruments ....................................................................................... 25

ATA Chapter 34: Navigation ................................................................................................................ 25

CONTACT INFORMATION....................................................................................................27

July 2007 Page 4


Summary

Introduction

This is a one-time inspection report issued by the International Bureau of Aviation (IBA Group) for a Boeing 737-500 aircraft, registration FAP-356 and serial number 27426, registered to the Peruvian Air Force, and delivered new from Boeing. The purpose of this report is to provide a pre-purchase report, covering the physical condition of the Boeing 737-500 and an overview of the condition and compliance of the aircraft records to enable IBA Group to provide an accurate Valuation. The report is made up of three sections, Section 1, the Physical Inspection Report, Section 2, the Aircraft Records Inspection and Section 3, an Avionics Status Report. History General

The aircraft was purchased new from Boeing by the Peruvian Government to be used solely as the Presidential transport. It was dispatched upon delivery to Associated Air Centre at Love Field Texas for the interior modifications. The aircraft was registered with the Peruvian Air Force as Registration No. FAP-356. Airframe and engine routine maintenance is carried out by the Air Force using its maintenance facility at Lima; heavy maintenance has been carried out by SEMAN and VARIG, which have been approved by the DGAC and FAA to carry out maintenance on the 737-500 aircraft. Records and documents relating to msn 27426 were made available to IBA at the Group 8 Air Force Base technical offices in Lima Peru. Technical Status

From the information gained during our inspection of this aircraft and its record on the 2nd, 3rd and 4th of July 2007, we have been able to make an assessment of the current maintenance status of msn 27426. At of the 03rd July 2007, the aircraft had completed 3,884.7 flight hours and 2,938 flight cycles since new. Recommendations

We have recommended that ProInversion apply to the DGAC to have the aircraft placed on the civil register and obtain a Certificate of Airworthiness (C of A), in order that an appropriate Export C of A may be issued to a prospective purchaser.

July 2007 Page 5


Section 1:

Physical Inspection Report

July 2007 Page 6


1.1 Inspection Conditions The aircraft was inspected in the SEMAN hangar at the Group 8 Air force base in Lima. The hangar was clean and well lit. 1.2 Physical Inspection

Cargo hold doors and Engine Cowls were opened to facilitate inspection. Emergency lighting and IFE equipment were function tested satisfactorily during the inspection. 1.2.1 Aircraft Manufacturers Data Plate & Owners Data Plate

Data Plate Information Manufacturers Model Number 7 Manufacturers

Serial Number 27426

Type Certificate Number A16WE Production

Certificate Number 700

Owners Data Plate Information

Not Fitted

1.2.2 Fuselage

The aircraft livery consists of a grey belly and lower surfaces (Air Force standard), white upper fuselage with blue stripes at the window line and two vertical red stripes on the rudder. The paint condition over all was very good. No repairs or dent damage were noted on the fuselage. There were some very minor paint chips at the forward service door cutout. In general the fuselage and paint condition was very good. 1.2.3 Empennage

Access was limited to the view from the ground but the skin appeared to be repair and damage free and the paint appeared to be in good condition. No leaks from the area were apparent. 1.2.4 Wings, Flaps and Control Surfaces

One area of repair encompassing an insert repair using blind fasteners and a patch repair was noted on the right hand leading edge Slat #5. This may be of concern to potential purchasers. Both wings upper and lower surfaces appeared to be damage free and the paint condition was very good. Apart from the repair the leading edges were in good condition and no dents or damage noted. Numerous minor dents on the inboard aft trailing edge flaps were noted. There was no evidence of leaks in the area. The Flaps were cycled during engine runs and Flight Control checks carried out for demonstration purposes.

July 2007 Page 7


1.2.5 Structure

All areas of structure on view, including keel beam section in the wheel well and areas visible in the E&E bay were all clean and corrosion free. 1.2.6 Landing Gear

All landing gears were very clean and appeared well lubricated. All clips, pipes, cables, and harnesses appeared to be in good condition and properly secured. It was noted that the wheel well areas did not appear to be treated with corrosion inhibitor. 1.2.7 Engines

Number 2 engine Lip Cowl had a small dent at the 7 o’clock position looking aft. There was also evidence of light surface corrosion on the skin due to moisture being trapped between the inlet covers and the skin, a result of the time the aircraft spends parked (see photos). All cowlings were in very good condition apart from some minor incidents of dull paint finish. Both Acoustic Panels and Abradable Linings were in good condition with no evidence of repairs or damage. Both exhaust areas were in very good condition as were both Pylons. No leaks were evident. Engine runs at Idle and High Idle were carried out for demonstration purposes. 1.2.8 Auxiliary Power Unit

No access. APU start-up from cold, and operation under pneumatic and electrical loads was observed. 1.2.9 Flight Deck

No reinforced cockpit door fitted. No cabin surveillance system fitted. The cockpit was clean and tidy with no evidence of damage to trim fittings. All seat covers were in good condition. Windows appeared to be in good order with no signs of crazing or delaminating noted. All instrumentation and radio equipment were in serviceable condition. IRS alignment checks, TCAS and EGPWS tests were conducted under observation as were function tests of Air Conditioning Packs. 1.2.10 Passenger Compartment The passenger compartment is divided into three areas. The forward section comprises of the forward Galleys, forward Lavatory, and the State Room Suite, the second (mid) area is the Business Class seating area and the aft area provides Economy (Coach) Class seating. The cabin attendants’ seats (1 pair forward and 1 pair aft) were in good order as were all harnesses but temporary seat covers had been fitted, which raise questions of Burn Certification, we have recommended their removal, as the originals are still apparently fitted underneath. The State Room Suite has four (4) burgundy leather Pullman seats on swivel mounts surrounding the collapsible table, with two (2) pairs of foldable jump seats on the left wall and a three-seat Divan at the compartments rear bulkhead. It also has a dedicated toilet suite complete with wardrobe, and an independent IFE system. The State Room is finished in a dark wood veneer with cream pile carpet

July 2007 Page 8


and cream suede effect ceiling covering with down-lighters. The wall panels are trimmed with burgundy and navy fabric. All were in good condition. The business class section of the cabin contains six (6) pairs of Business Class seats finished in blue leather and all in good condition. The carpet is cream and in good condition. Ceiling mounted monitors provide IFE. The aft cabin section provides forty-two (42) Economy (Coach) Class seats covered in Burgundy fabric. All cabin sidewall floor covering and ceiling panels and window scratch panels were in good condition.

Cabin Equipment

Description Number Installed Manufacturer Manufacturers

Model Number Manufacturers Part Number

Flight Attendant Seats 2 Pairs Burns Not Known S414N201-525CRS414N201-533CR

Entertainment System 2 Refer Fit List Refer Fit List Refer Fit List First Class Seats 4 Not Known Not Known Not Known Divan Seats 1 Not Known Not Known Not Known Business Class Seats 12 BE Aerospace 940 S403706-401/402Economy Class Seats 42 BE Aerospace 940 S403707-403/404

Emergency Escape Slides Rafts

4 2

Air Cruisers 61621-469

Hoover E52/4600-103

Slides-Each entry door (x4) Rafts- Fwd LH cabin stowage

Disabled Access Seat No N/A N/A Movie System Installed Yes Ceiling MAS Air-phone Installed Yes / No No Data Has been removed from jack point Language(s) of Cabin Placards Spanish / English Location of Passenger Life Vests Under seats / Stowage Compartments

Location of Lavatories 1 Fwd Cabin 1 Aft Cabin 1 State Room

Type of E-Path Lighting Floor Lighting single strip

July 2007 Page 9


Cockpit Equipment List

Location Equipment Description Manufacturers Model Number

Manufacturers Part Number

F/O Bulkhead Fire Extinguisher Kidde Halon 1211 898052 Pedestal Flashlight DME Corp P2-07-001

Rear of Seats Crew Life Vest KSE-35L8 P0723E105PWC

Side Panel Smoke Goggles Not Known Not Known

Behind Capt. seat PBE Scott 822300-14

Cabin Equipment List

Location Equipment Description Manufacturers Model Number

Manufacturers Part Number

Fwd & Aft C/A stations Under Seats

Crew Life Vest Pax Life Vests

KSE35L8

P0723E105PWC/ - 125W

Cockpit Seat Row 9 Bin PBE

Puritan Bennett 16827

119003-11

Cockpit C/A Seat

Flash light DME P2-07-0001-214

Seat Row 9 Bin Gloves Not Known Not Known

Fwd LH Cabin Aisle Storage ELT

Dayton Granger EB-2BW-Dolphin

75056-J

Seat Row 9 Bin Fwd LH Cabin Aisle Storage

Oxygen Bottle Scott DOT3AA1800-BUA-BF23

Fwd LH Cabin Aisle Storage Life Raft Hoover FR46 E52/4600-103

Seat Row 1 Bin Seat Row 9 Bin

Fire Extinguisher Kidde Halon 1211 898052

Seat Row 9 Bin Megaphone ACR No Data Seat Row 9 Bin First Aid Kit DME Corp. S6-01-005-301

1.2.11 Galleys and Lavatories

The Galley areas are clean and appear to be little used. The flooring is of a mini-coin mat type and is in good condition and is well sealed against moisture ingress. Both forward and aft lavatories are clean, in good condition and are fitted with stainless-steel sinks.

July 2007 Page 10


Galley Equipment



Galleys 5 Muhlenburg Refer Fit List Refer Fit List Ovens 3 Burderus Sell Not Known 8201-11-0000

Galley Locations G1 (RH Fwd) G2 (RH Fwd) G3 (RH Aft) G4 (RH Aft) G6 (LH Aft)

1.2.12 Equipment Compartment

The equipment bay was clean and visible structure appeared to be damage and corrosion free. 1.2.13 Cargo Compartments

The cargo bays were extremely clean and appeared to free of damage to floors bulkheads or sidewalls. A 1000 Gal two part Aux tank is fitted in the Aft Cargo Bay. 1.3 Conclusion The cabin layout with forward and aft galleys and forward and aft lavatories lends itself to easy conversion back to a full passenger configuration. It should also be noted that the original all passenger configuration ceiling and sidewall panels were retained and are included in the spare parts package available with the aircraft. This aircraft is in an exceptional condition and has had extremely low usage. The Landing Gears are newly overhauled. The aft Aux Tank (Aft Cargo bay) is temporarily deactivated awaiting Boeing feedback on a related Service Bulletin.

July 2007 Page 11


Section 2:

Aircraft Records Inspection

July 2007 Page 12


General Aircraft Description Manufacturer / Model Boeing 737-528 Manufacturer Serial Number 27426 Current Registration FAP-356 Line Number 2739 Variable Number PT 517 Date of Manufacture June 1995 Registered Owner Fuerza Aerea Del Peru F.A.P. (Peruvian Air Force) Country / National Authority Peru / DGAC Current or Last Operator F.A.P. Date of Delivery to Current Operator 29th November 1995 ETOPS Equipped Yes (not certified)

Aircraft Utilisation

As of Date: (03/07/2007) Airframe Total This Month

Hours Cycles Hours Cycles

3882 2936 0 0

Certified Operating Weights Weights Pounds Kilograms

Maximum Taxi Gross Weight 134,000 60,781 Maximum Take-Off Weight 133,500 60,554 Maximum Landing Weight 110,000 49,895 Maximum Zero Fuel Weight 102,500 46,493 Basic Empty Weight 72,000 32,659 Aircraft Last Weighed 26th August 2006

Maintenance Program

Maintenance Schedule Reference Number Boeing MPD D6-38278 Airworthiness Approval Number N/A Program Based on Utilisation of: Low Hours 600 FH / Year Fuel Tank Contamination Prevention Program No Period N/A Aircraft Wash Program Yes Period Every 4 days Engine Trend Monitoring No Period N/A Engine Vibration Monitoring Yes Period Per Flight Engine / APU Compressor Washing Yes Period Every 2A Check / 2 Months

July 2007 Page 13


Maintenance Schedules and Status As of Date: (03/07/2007)

Check A

Frequency Calendar 2 Months

Hours N/A

Cycles N/A

Last Accomplished Date

18/05/2007 Total Hours

3878 Total Cycles

2921

Next Due Calendar

18/07/2007 Hours

N/A Cycles

N/A

Check

C

Frequency Calendar 2 Years

Hours 4000

Cycles N/A

Last Accomplished Date

29/08/2006 Total Hours

3809 Total Cycles

2832

Next Due in Calendar

28/09/2009 Hours 7809

Cycles N/A

Structural Significant Items SSI Threshold As Per MPD

SSI Re-Inspection Frequency As Per MPD

July 2007 Page 14


Titled Engines

Model Description Pos. Manufacturer Manufacturers Part Number

Engine Location

CFM 56-3C-1 1 CFMI CFM56-3C-1 MSN 27426

Engine Serial Number: 858237 Description As of date Hours Cycles

Engine Total Time (TSN / CSN) 03/07/2007 3884.7 2938 Engine Time at Current Installation 22/06/1995 0 0 Time Since Current Installation - On Wing 03/07/2007 3884.7 2938 Time Since last shop visit N/A N/A N/A Remaining Time to First Life Limiter (Compressor Rear Air CPD Seal) 03/07/2007 N/A 12062

Titled Engines

Model Description Pos. Manufacturer Manufacturers Part Number

Engine Location

CFM 56-3C-1 2 CFMI CFM56-3C-1 MSN 27426

Engine Serial Number: 858238 Description As of date Hours Cycles

Engine Total Time (TSN / CSN) 03/07/2007 3884.7 2938 Engine Time at Current Installation 22/06/1995 0 0 Time Since Current Installation - On Wing 03/07/2007 3884.7 2938 Time Since last shop visit N/A N/A N/A Remaining Time to First Life Limiter (Compressor Rear Air CPD Seal)

03/07/2007 N/A 12062

July 2007 Page 15


Auxiliary Power Unit (APU)

Manufacturer Model Number Manufacturers Part Number

Manufacturers Serial Number

Hamilton Sundstrand T-62T-47C1 170101-106B SP-E952471

APU Status Description As of date Hours Cycles APU Manufactured Date 24/05/1995 Total Time Since New (TSN) 03/07/2007 4727 4794 Aircraft Hrs / Cyc at APU Installation 10/01/2007 3878 2919 APU Life at Installation 10/01/2007 4718 4778 APU Time Installed on Aircraft 03/07/2007 9 16 APU Hot Section Inspection (HSI) Period O/C N/A N/A APU Overhaul (OH) Period O/C N/A N/A APU Time Since Last Shop Visit 28/11/2005 162 214 APU Time Since Hot Section Inspection 03/05/2007 N/A N/A

July 2007 Page 16


Landing Gears Nose Landing Gear P/N: 65-46200- 80 S/N: T5450P2739

Landing Gear Time since new As of date 03/07/2007

Hours 3884

Cycles 2938

Last Overhaul Date Calendar

21/07/2006 Hours 3809

Cycles 2832

Overhaul Interval – Operator (TBO) Years

10 Cycles 20,000

Time remaining As of date 03/07/2007

Years / Months 9 Years

Cycles Not Known

Landing Gears Left Main Landing Gear P/N: 65-46100-79 S/N: MCO5465P2739


Hours 3884

Cycles 2938


21/07/2006 Hours 3809

Cycles 2832


10 Cycles 20,000



Cycles Not Known

Landing Gears Right Main Landing Gear P/N: 65-46100-79 S/N: MCO5466P2739


Hours 3884

Cycles 2938


21/07/2006 Hours 3809

Cycles 2832


10 Cycles 20,000



Cycles Not Known

July 2007 Page 17


Fuel Fuel Tanks Fuel Capacity Pounds Fuel Capacity Kilograms

Left Wing Main 1499 1248 Right Wing Main 1499 1248 Center 2313 1926 Aux Tank Aft Cargo 1000 833 Total Fuel 6311 5255

Equipment and Furnishing



Flight Attendant Seats

1 Fwd Pair 1 Aft Pair

Burns Not Known S414N201-525CRS414N201-553CR

Galley Unit G1 1 Muhlenberg N/A RR97101-35-1 Galley Unit G2 1 Muhlenberg N/A 106074 Galley Unit G3 1 Muhlenberg N/A 106076 Galley Unit G4 1 Muhlenberg N/A 105124 Galley Unit G6 1 Muhlenberg N/A 106073 IFE System (Pax Cabin) 1 Matsushita Not Known RD-AV 3001-31

IFE System (Presidential Suite) 1

Sony (VCR/Tuner/Amp)

Philips (DVD) Bose (Speakers)

Not Known

Not Known Acustimass AMS

SLV-R1000/ST-S211ES/TAF606

DVD736K Not known

Tape Reproducer 1 Matsushita Not Known RDAX7670 First Class Seats 4 Not Known Not Known Not Known Business Class Seats 12 BE Aerospace 940 S403706-401/402Economy Class Seats 42 BE Aerospace 940 S403707-403/404Ovens 3 Buderus Sell Not Known 8201-11-0000

Primary Overhaul Agencies Airframe Varig, SEMAN. Engines Varig, SEMAN Auxiliary Power Unit Honeywell Landing Gear Goodrich Avionics Vendor

July 2007 Page 18


Deferred Defects Number of Deferred Defects 4

Date of Oldest Entry 2nd April 2007 (Seat 10F Audio Inop.)

Aircraft Modifications and STC’s STC / Modification Number Description

ST 00899AT Installation of CAS-18 TCAS

SA 725 NE Installation of 1000 GAL 2 tank AUX Fuel System in Aft Cargo Compt. Note: AD Pending (over run) to de-activate

July 2007 Page 19


Aircraft Operations Manuals The aircraft operational manuals were inspected and found to be at the following revision standard

Aircraft Operations Manuals

Manual Title Revision Number Date

Operations Manual /FCOM /QRH 16 08/06/2007 AFM 7 12/01/07 AMM 29 12/01/07

Airworthiness Directives

Outstanding Airworthiness Directives AD Number Description Due at:

99-08-23 Detect and correct fatigue at fastener holes at the rear pressure bulkhead. 25,750 Cyc

2000-07-06 Prevent fatigue cracking of the lower corners of the door frame and cross beam of the forward cargo door 13,519 Cyc

2001-02-01 Detect fatigue cracking of the forward pressure bulkhead 20,000 Cyc

2001-04-06 Lubricants no longer approved. Fan Disc Dovetail wear check 20,000 Cyc

2002-10-12 Prevent Aileron Tab from disconnecting 5,799 FH 2003-14-06 Detect and correct fatigue cracks in lap joints 20,000 Cyc

2004-06-18 Replace valve seals and perform leak checks 7,697 FH 8,197 Cyc

2004-10-06 Hydraulic Heat Exchanger 27/05/2009 2004-15-04 Fueling Float Sw wiring in centre tank 30,000 FH

2005-07-19 Detailed visual inspection and Low Mid and High Frequency Eddy Current 4,000 Cyc

2005-13-15 Detailed inspection for discrepancies of the secondary vapour barrier 27/07/2009

2005-13-27 Detailed and Eddy current inspection for cracking of the crown area of the fuselage skin 21,000 FH

2005-19-25 Eddy Current around satellite holes of the Rad Alt 20,000 Cyc 2005-20-01 Detailed inspection of stiffeners at LBL and RBL 6.5 20,000FH 2005-20-03 Detailed Inspection of Intercostal Web 15,000 FH 2005-23-17 Detect and correct chafing at P-15 fueling panel Overdue 2005-26-03 Prevent loss of Elevator control 20/01/2011

July 2007 Page 20


Outstanding Airworthiness Directives AD Number Description Due at:

2006-03-12 Inspect for chafing of wire bundles above centre fuel tank 16/03/2011

2006-18-11 De-activation of Aux Fuel Tank Overdue 2006-07-12 Scribe marks on lap joints 15,000 Cyc 2006-21-01 Prevent excessive airframe vibration 15/09/2007 2006-26-09 Fuselage Air Con Bracket attachments 7573 Cyc

Repetitive Airworthiness Directives AD Number Description Due at:

99-21-15 Detect and correct chafing & prevent electrical arcing at the fuel boost pump 32,398 FH

2000-07-06 Prevent fatigue cracking of the lower corners of the door frame and cross beam of the forward cargo door 6,019 Cyc

2002-01-01 Prevent excessive in flight vibration of the elevator tab 5,236 FH 3,944 Cyc

2002-10-11 Detect and correct corrosion or cracking of the aft pressure bulkhead at BS 1016 02/01/2008

2003-26-01 Bolts in Rudder Front Spar Main Thrust Hinge, Actuator Assy and Support Fitting

5,197 FH 3,970 Cyc

2004-19-10 Horizontal Stab Pivot Pins 08/08/2008 2004-22-05 Dorsal Fin Assy 11,383 Cyc

Appliance and Engine Airworthiness Directives

Appliance Airworthiness Directives AD Number Description Due at:

Not Available from operator during this Inspection

Engine Airworthiness Directives AD Number Description Due at:

97-08-01 Prevention of low cyclic failure of fan disc 17162 Cyc 2002-13-03 Detail specific inspection to prevent critical parts failure 12062 Cyc

2006-26-01 Fuel filter replacement with specific pt/no( not identified on provided data sheets)

Next fuel filter change or 4,000 hours since

issue of AD

July 2007 Page 21


Aircraft Damage Chart The following table gives details of those items recorded where, in the opinion of the surveyor; there was insufficient documentation to confirm sign off in accordance with manufacturer approved documentation.

Aircraft Damage Chart Repair Reference Comments

Not Available from operator during this Inspection Hard Time Components Listing Please refer to the supporting documents for a copy of the Hard Time Components Listing

July 2007 Page 22


Documents List

The following documents were checked with the aircraft Yes / No

1 Airframe Log Book(s) Yes 2 Engine Log Book(s) Yes 3 Auxiliary Power Unit Log Book(s) Yes 4 Modification Log Book(s) No 5 Technical Log / Journey Log No 6 Certificate of Registration No 7 Certificate of Airworthiness No 8 Noise Certificate No 9 Radio License No 10 Insurance Certificate Yes 11 Weight and Balance Schedule No 12 Hard Time Component Listing Yes 13 Engine Disc Sheets Yes 14 AD (Airframe) Listing Yes 15 AD (Engine) Listing Yes 16 AD (Appliances) Listing Yes 17 SB (Airframe) Listing Yes 18 SB (Engine) Listing Yes 19 SB (Equipment) Listing Yes 20 LOPA & Safety Equipment Yes 21 Avionics Equipment List Yes 22 Deferred Maintenance Items Yes 23 Maintenance Program Yes 24 CPC Program Yes 25 Flight Manual Yes 26 Crew Manual Yes 27 MEL / CDL / DDG Yes 28 Weight and Balance Manual Yes 29 Flight Test Reports No 30 Mandatory Occurrence Reports No

July 2007 Page 23


Section 3:

Avionics Status Report

July 2007 Page 24


ATA Chapter 22: Auto Flight



Flight Daa Loader 1 Allied Signal Not Known 964-0401-016 Mode Control Panel (MCP) 1 Honeywell Not Known 4051601-939 MCDU 1 Smiths Not Known 170089-02-01 TMA 1 ADS-INC Not Known 10-62058-7 Integrated Flight system Assy Unit 1 Boeing Not Known 65-52820-2 ASA 2 Boeing Not Known D434-56-001 Yaw Damper Coupler 1 Honeywell Not Known 4084042-911 Autothrottle Servo Actuators 2 Smiths Not Known 111 RAA 3 IRU 2 Honeywell Not Known HG1050 AE09 Auto Throttle Computer 1 Smiths Not Known 733-SUE-2-4 Digital Analog Adaptor 2 Honeywell Not Known DG1035AB03 Mode Selector Unit 1 Honeywell Not Known 69-73713-17 Flight Control Computer (FCC) 2 Honeywell Not Known 4051600-914 Flight Management Computer (FMC) 1 Smith Not Known 176200-01-01 VSI 2 Honeywell Not Known 4039893-903 GPS Sensor Unit 1 Honeywell Not Known S242T104-101

ATA Chapter 23: Communication



HF Comms Transceiver 1 Collins Not Known 622-5272-120 VHF Comms Transceiver 3 Honeywell Not Known 064-50002-0101 Passenger Address (PA) Amplifier 1 Collins Not Known 622-4096-001 Remote Electronic Unit 1 Avtech Not Known 5140-1-1 Audio Control Panel 3 Avtech Not Known 5145-1-66 Music Announce Control Panel 1 Matshushita Not Known RD-AX 7670 Music Announce Control Panel 1 Panasonic Not Known DRAX7681 Decodificador Selcal 1 Team Not Known SC2253ADO Control Panel 3 Boeing Not Known 285 U0037-617 Coupler Antenna 1 Collins Not Known 792-614D-601

July 2007 Page 25


ATA Chapter 27: Flight Controls



Test Stall 1 Boeing Not Known 69-75978-1 Yaw Damper Indicator 1 Ametek Not Known 253884 Flight Recorder Module 1 Boeing Not Known 69-37325-137 Stall Management Computer 1 Boeing Not Known 6552-828-7

ATA Chapter 31: Independent Instruments



Cockpit Vioce Unit 1 Fairchild Not Known 93-A100-80 Aural Warning Unit 1 Boeing Not Known 69-78214-1 Control Panel 1 Loral System Not Known 93-A152-20 Digital Flight Data Acquisition Unit (DFDAU) 1 SFIM INC Not Known ED44B409

Digital Flight Data Recorder (DFDR) 1 SFIM INC Not Known AP41116101

ATA Chapter 34: Navigation



GPWS Computer 1 Allied Signal Not Known 965-0976-003-105-105

GPWS Control Panel 1 Boeing Not Known 69-37369-24 VOR/ILS Receiver 2 Collins Not Known 822-0761-001 Control Panel VHF NAV/DME 2 Boeing Not Known 65C35322-1 RDDMI 2 Honeywell Not Known 4034559-911 Receiver Marker Beacon 1 Collins Not Known 522-2996-011 Receiver ADF 1 Collins Not Known 777-1492-005 Control Panel ADF 1 Collins Not Known 792-6275-005 Transceiver Radar 1 Collins Not Known 622-5132-109 Radar Control Panel 1 Collins Not Known 622-5129-105 Radar Antenna 1 Collins Not Known 622-5137-001 DME Interrogator 2 Collins Not Known 622-4540-122 ATC Transponder Mode S 2 Collins Not Known 622-7878-201 CTA-81A Control Panel 1 Honeywell Not Known 071-01-503-2601 TCAS Processor Enhanced TPA-81A 1 Honeywell Not Known 066-50000-2220

July 2007 Page 26


ATA Chapter 34: Navigation



Transceiver Radio Altimeter 2 TRT Not Known 95-99-607-14931 Air Data Computer 2 Honeywell Not Known 4061100-901 Altimeter 2 Smiths Not Known 2056-01-1 Mach/Air Speed Indicator 2 Smiths Not Known 2083-11-1 EADI 2 Collins Not Known 622-7998-013 EHSI 2 Collins Not Known 622-7999-013

Is Windshear System Installed? Yes

Yes Is it part of the GPWS System? Is it part of the Radar System? No Altimeter Indictors Feet

July 2007 Page 27


Contact Information

Company Address

ProInversion Asesor Técnico Proyecto de Aeropuertos

Name: Bruno Leoni Title: Asesor Técnico

email: [email protected] Tel: 612-1200 ext 1346 Fax:

Name: Title:

email: Tel: Fax:

Signed: Date: 06 July 2007 John Donnelly Technical Manager

Approved: Alan Miles Director, Asset Management & Continuing Airworthiness Manager

IBA Group Limited has performed a survey of this aircraft and records. The extent of survey is limited to walk around inspection without removal of access panels unless specifically noted. Engines and APU are not borescope inspected or performance checked. Aircraft systems performance and aircraft handling is not checked unless specifically noted. Aircraft records are as presented by the current aircraft managers. The survey collates data from many sources outside of IBA control. IBA Group Limited, its associated companies, subsidiaries, Directors and employees are not liable for errors and omissions.