“keep in full force and effect … hull, passenger, breach of warranty, war risk and other insurance in such form and substance as satisfactory to Grecoair. Grecoair shall be named as loss payee on Hull insurance …. AAC agree to furnish Grecoair with a certificate of insurance therefore including such insurance carried by AAC which shall include Grecoair as Co-Insured for respective rights and interests under the Aircraft Liability Coverage.”
“The Insurer shall, at his discretion, pay for, replace or make good any loss or accidental damage to the aircraft described in the Declarations resulting from the risks covered ….”
“the provisions of the lease agreement existing between AAC and Grecoair are included, in accordance with the content of the Airline Finance/Lease Contract Endorsement clause (AVN 67A) attached.”
“Original Policy … with: 7. In respect of [the aircraft] agree include provisions of dry lease agreement with Grecoair (as expiry) and in this respect include … AVN 67A …. Grecoair are held harmless in respect of any/all losses of or damage to the aircraft for the duration of the lease ….”
“(a) no amendment to the terms or conditions or additions to or deletions from the original policy shall be binding upon Reinsurers hereon unless prior agreement has been obtained from the said Reinsurers; (b) the Reinsured shall upon knowledge of any loss … advise the Reinsurers within 72 hours; (c) the Reinsured shall furnish the Reinsurers with all information available respecting such loss … and the Reinsurers shall have the sole right to appoint adjusters, assessors, surveyors and/or lawyers and to control all negotiations, adjustments and settlements in connection with such loss …”
“Information: Original policy … wording with (inter alia): (2) This Policy to follow all the terms and conditions of the Aircraft Hull All Risks Policy.”
“Reinsurers have agreed to include the insurance requirements of such Agreement in the Policies of Reinsurance in relation to this aircraft, subject to … AVN 67A as attached: Pursuant to the insurance and indemnity requirements of the lease Agreement Reinsurers have agreed to: (a) Hold harmless and waive rights of subrogation against Grecoair in respect of any/all loss or damage to the aircraft for the duration of the lease. (b) USA Jurisdiction Clause.”
“The aircraft is the subject of a Dry Lease (“Agreement”) … between Grecoair … and The Insured and Reinsurers have agreed to the following Insurance requirements of the Agreement being included in the Policies of Insurance in relation to the aircraft: 1. Under the Hull All Risks and Hull War Risks Policies: a) Grecoair Inc is included as loss payee. b) Agreement to indemnify and hold harmless Grecoair Inc in respect of any/all loss of or damage to the aircraft for the duration of the lease, but subject always to the policy period of the insurance. …. The original policy has been endorsed with … AVN 67A under which the “Contract Parties” are Grecoair ….” b) Agreement to indemnify and hold harmless Grecoair Inc in respect of any/all loss of or damage to the aircraft for the duration of the lease, but subject always to the policy period of the insurance. …. The original policy has been endorsed with … AVN 67A under which the “Contract Parties” are Grecoair ….”
“It is common practice for a certificate of reinsurance to be issued as a means to prove that the underlying insurer has purchased valid reinsurance in the international market.”
“a. The severing of eight right hand circumferential frames just above the main deck cargo floor at Stringer 17R from station 480 through to 600D. b. The fuselage skin was punctured in 2 places with the skin protruding outwards between station 580 and 600D immediately above Stringer 17R. c. Further damage was suspected to major structural components bearing in mind that such damage had occurred opposite the main cargo door and above the front baggage door into the hold.”
“13. Paragraph 18 is not admitted. Further, the damage which is alleged to have been caused by the First Accident is common amongst Boeing 707 aircraft, and is caused by distorted pallets riding over the side guidance rails when the pallet is being loaded. This type of damage can be caused by one accident or by a cumulative effect of several incidents. Given the late notification, set out below, the First Defendant is prejudiced in its ability to investigate the cause of the alleged loss, and reserves the right to plead further once disclosure has been provided of the maintenance history of the Aircraft. Accordingly, the Claimant is required to prove the First Accident and the precise damage that was caused by the First Accident. 14. Further, as the First Accident was notified to the First Defendant after a considerable period of delay, namely in about early February 1996, the First Defendant reserves the right to rely on any defence available to it or ENSA for late notification, once it has seen the 94/95 ENSA Policy.”
“19. On8 April 1995 , while the Second and Third Defendants were on risk, and the Aircraft was being operated by AAC pursuant to the Lease, the Aircraft was stationary at Saurimo Airport Angola. While the Aircraft was parked a truck collided with the aft end of the fuselage causing damage to the Aircraft. The accident occurred shortly after 0845 hours (“the Second Accident”). 23. The Second Accident caused damage to the aft fuselage: a. Skin impact damage was visible at station 1300 to station 1400 left hand lower side. b. There were signs beyond the above areas exhibiting signs of outward stress. c. A skin crack of approximately 3 inches at station 1343 above Stringer 17L indicated that more damage was hidden. d. Permanent wrinkles could be seen extending forward and aft of the impact area. This suggested severe damage to the main rear bulkhead, four secondary rear bulkheads. e. The original skin was punctured profusely in the skin layers between the frames at stations 1300, 1320, 1340, 1360, 1380. f. Four circumferential frames at Stations 1320 to 1380 were severed at or near Stringer 24L. g. All the Stringers in the impact area and forward and aft were distorted and fractured. h. The above damage was suggestive of structural damage caused in other areas.”
“The condition of the aircraft in general was found to be lacking in proper maintenance, there was significant lack of corrosion control in evidence. Listed here are some of the discrepancies observed. Along the fuselage belly, the skin exhibited extreme bulging typical of corrosion damage. Body cutouts for antennas and access panels were severely corroded around the periphery. Lower lobe skin lap and circumferential joints showed signs of significant corrosion damage. At STA good on the left hand side at STR 24, there is a 6 inch long crack common to the upper row and 3 inch long crack common to the middle row. Skin and doubler disbond could be seen along the cutouts of the nose landing gear wheelwell, the forward entry door and the lower lobe cargo doors. Local to the aircraft body impact damage, a skin crack approximately 3 inches in length immediately above stringer 17L at STA 1435. The main deck cargo floor was in severe distress, floor panel punctures and seat track damage including seat track lip cracks and corrosion could be seen. All nose landing gear and main landing gear tires were severely worn. Significant corrosion is evident on the ribs and lugs of the nose landing gear. …. Our observations suggest that the structural integrity of the aircraft is compromised. We are also of the opinion that the airplane is also out of compliance with the 707 corrosion protection and control program. Further, the condition of the structure calls into question the aeroplane’s status with regards to the ageing fleet program mandatory inspections and mandatory modifications. We consider the airplane not airworthy in its current state. We strongly recommend that the airplane undergo an inspectionequivalent to that accomplished during a complete D-Check. All damage found needs to be addressed and repaired in accordance with the structural repair manual requirements and/or in accordance with the manufacturer’s or aircraft industry approved repair methods. …. We wish to point out that we are obligated to report to the FAA of an airplane that is operating in a non-airworthy condition. Consequently, we need to know your plan to address the structural integrity of the aircraft prior to further flight of airplane D2-TOR. Should any assistance be required in formulating the necessary repairs, please contact us with a detailed description of the damaged areas and we will provide repair instructions for each area.”
“From what we know, we would expect to have to replace frames or frame sections, skins, stringers and doublers in the damaged areas. We are required under our FAA Repair Station License to completely restore the structural integrity of the area we repair. With this in mind, we anticipate requiring a team of 32 people on site for 30 days. The team would consist of 24 mechanics; 2 manufacturing team capains (sic), 2 Quality Assurance supervisors, 2 tooling and 2 structures engineers. The price to cover such a team is reflected below. On-site Labor and Subsistence: 32 people for 30 days:$2,563,200 Labor and Subsistence for Travel to and from the Repair Site: 32 people for 3 days: 184,320 Round-trip Business Airfares to and from the Repair site: 32 x Approx.$4500 144,000 Preliminary Estimate for Parts and Materials 300,000 Estimate of Freight and Handling for Parts, Materials, Tools and Equipment 120,000 Total$3,311,520 ”
“1. In view of the extent of damage and the repair required to the aircraft, major disassembly and replacement of the fuselage structure will be required. Accordingly the aircraft has to be hangared, shored and jigged to proper alignment position. Thus the aircraft has to be ferried to GAMCO. Our estimate does not cover expenses associated with the ferry flight nor the cost of preparation of the aircraft for ferry flight. 2. As detailed in paragraph (A)3.17 above there is a pronounced wrinkle at the RH lap joint BS 1430 stringer 10 area. Complete disassembly & removal of skin will be required to determine the actual extent of damage to this area. Our estimate does not cover this area and any findings associated with this damage. 3. There are corrosion indications in several areas. These are not costed out as the scope of work does not include such work.”
“Underwriters would be prepared to offer US$ 250,000 in full and final settlement of this claim subject to a release and discharge ….”
“The meeting ended. 5 minutes later Mr Bolshaw called to say that they would like the aircraft repaired.”
“Mr Tokoph said that he was not accepting Maria Cetta’s offer and had decided to opt for repairs to the aircraft.”
“It became apparent during the meeting that it was impossible to agree on the quantum of the claims as our belief is totally different to that of Re-insurers in that we do not believe the aircraft can be repaired for the sum they have offered. Maria Cetta said they were perfectly happy to repair the aircraft using FLS who Lloyd’s Aviation had obtained repair estimates from. We have therefore decided that this is the only option available for an amicable settlement to be reached. Please therefore proceed to having the aircraft repaired as soon as possible and keep us advised as to when this work will proceed. We expect the aircraft to be repaired in accordance with the manufacturers recommendations and to be FAA approved. The condition of the aircraft once repaired needs to be at least as good as it was prior to the damage occurring. We do appreciate however that we are only dealing with the accidental damage and not other items.”
“… The deductible underwriters were advised by their agents that, even if the two areas of damage were repaired, the aircraft was unlikely to fly again due to the extensive amount of corrosion to the fuselage …. … underwriters would like to conduct a detailed review of the alternative repair estimates before making a decision as to where and how the aircraft is to be repaired. There is a very real prospect that the aircraft may not be moved due to the extent of the non-accident related damage either before or after it has been repaired. As you have expressly pointed out, underwriters will only be responsible for accident related damage. Please advise what proposals you have to effect all non-accident related damage repairs as underwriters would wish to test the aircraft as soon as these non-accident related areas have been repaired Any settlement will be conditional upon a release and discharge being signed by all relevant parties and you are unlikely to sign the same until a full flight test has been carried out. Unless you are able to confirm the precise dates on which you propose to effect repairs, underwriters may consider deferring authorising repairs until you are in a position to provide them with a date as they are concerned that the aircraft may be beyond economic repair due to the extensive non-accident related damage.”
“may we please have an answer to the question raised in our letter of 25th March. When are you proposing to repair the non-accident related damage?”
“… we confirm that no agreement has been reached between Grecoair and Lloyd’s Aviation on the 11 March ’97, in fact no agreement has yet been made to this date regarding the insurance of this aircraft. We remind you of our valid claims for damages suffered to our aircraft while operated by AAC and reaffirm our rights under the policy to claim from you up to a maximum limit of USD 4,500,000 …. As this settlement is long overdue, we urge you and your Lloyds partners to immediately repair the aircraft.”
“If settlement on this basis is not acceptable to Grecoair, then arrangements will be made for FLS … to undertake the repairs to the aircraft.”